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- 1982 NASA Space Biology accomplishments
- 1983-84 NASA space biology accomplishments
- 20th Aerospace Mechanisms Symposium : proceedings of a symposium cosponsored by National Aeronautics and Space Administration, the California Institute of Technology, and Lockheed Missiles and Space Company, Inc., and hosted by Lewis Research Center, May 7-9, 1986
- A Bibliography of planetary geology principal investigators and their associates, 1980-1981
- A Calibration technique for a hot-wire-probe vector anemometer
- A Method for obtaining reduced-order control laws for high-order systems using optimization techniques
- A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel
- A Pulse-forming network for particle path visualization
- A Study of production of miscibility gap alloys with controlled structures
- A System for aerodynamic design and analysis of supersonic aircraft
- A T-matrix theory of galactic heavy-ion fragmentation
- A bibliography of electrothermal thruster technology, 1984
- A bibliography of electrothermal thruster technology, 1984
- A bibliography of planetary geology principal investigators and their associates, 1982-1983
- A blackbody-pumped CO2-N2 transfer laser
- A chemical kinetic mechanism for the ignition of silane/hydrogen mixtures
- A class of nonideal solutions
- A closed-form solution for noise contours
- A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance
- A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis
- A comparative look at sunspot cycles
- A comparative statistical study of long-term agroclimatic conditions affecting the growth of U.S. winter wheat : distributions of regional monthly average precipitation on the Great Plains and the State of Maryland, and the effect of agroclimatic conditions on yield in the state of Kansas
- A comparison of the V/STOL handling qualities of the VAK-191B with requirements of AGARD report 577 and MIL-F-83300
- A comparison of two position estimate algorithms that use ILS localizer and DME information : simulation and flight test results
- A computer program for estimating the power-density spectrum of advanced continuous simulation language generated time histories
- A computer program for the generation of logic networks from task chart data
- A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft
- A conceptual framework for using Doppler radar acquired atmospheric data for flight simulation
- A constitutive model for the inelastic multilaxial cyclic response of a nickel base superalloy René 80
- A critical examination of stresses in an elastic single lap joint
- A design approach to real-time formatting of high speed multispectral image data
- A diagnostic model for studying daytime urban air-quality trends
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
- A finite difference solution for the propagation of sound in near sonic flows
- A flight-test and simulation evaluation of the longitudinal final approach and landing performance of an automatic system for a light wing loading STOL aircraft
- A general aviation simulator evaluation of a rate-enhanced instrument landing system display
- A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies
- A low energy electron magnetometer
- A method for data base management and analysis for wind-tunnel data
- A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification
- A method for obtaining practical flutter-suppression control laws using results of optimal control theory
- A method of calculating the total flow from a given sea surface topography
- A method to stabilize linear systems using eigenvalue gradient information
- A microprocessor-based table lookup approach for magnetic bearing linearization
- A mobile work station concept for mechanically aided astronaut assembly of large space trusses
- A model for reaction rates in turbulent reacting flows
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- A new NASA/MSFC mission analysis global cloud cover data base
- A new look at numerical analyses of free-edge stresses in composite laminates
- A new look at numerical analyses of free-edge stresses in composite laminates
- A new measurement method for separating airborne and structureborne noise radiated by aircraft-type panels
- A new method for determining acoustic-liner admittance in a rectangular duct with grazing flow from experimental data
- A new methodology for free wake analysis using curved vortex elements
- A new sun : the solar results from Skylab
- A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane
- A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane
- A potential-energy scaling model to simulate the initial stages of thin-film growth
- A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
- A preliminary study of numerical simulation of thermosolutal convection of interest to crystal growth
- A procedure for designing forebodies with constraints on cross-section shape and axial area distribution
- A radionuclide counting technique for measuring wind velocity
- A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A rate-controlled teleoperator task with simulated transport delays
- A repair technology program at NASA on composite materials
- A review of some head-up display formats
- A simple model of space radiation damage in GaAs solar cells
- A simulation study of crew performance in operating an advanced transport aircraft in an automated terminal area environment
- A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise
- A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise
- A solution procedure for behavior of thick plates on a nonlinear foundation and postbuckling behavior of long plates
- A spatial model of wind shear and turbulence for flight simulation
- A stability analysis of AVE-IV severe weather soundings
- A stochastic model for photon noise induced by charged particles in multiplier phototubes of the space telescope fine guidance sensors
- A study of crystal growth by solution technique
- A study of resonant-cavity and fiberglass-filled parallel baffles as duct silencers
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
- A summation and inhibition model of annoyance response to multiple community noise sources
- A survey of nested grid techniques and their potential for use within the MASS weather prediction model
- A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects
- A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet
- A tutorial solution to scattering of radiation in a thin atmosphere bounded below by a diffusely reflecting, aborbing surface
- A unique facility for V/STOL aircraft hover testing
- A user-oriented and computerized model for estimating vehicle ride quality
- A variational assimilation method for satellite and conventional data : development of basic model for diagnosis of cyclone systems
- AESOP : an interactive computer program for the design of linear quadratic regulators and Kalman filters
- Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures
- Acceleration of convergence of vector sequences
- Acoustic facilities for human factors research at NASA Langley Research Center : description and operational facilities
- Acoustic measurements of the X-wing rotor
- Adaptive identification and control of structural dynamics systems using recursive lattice filters
- Adaptive identification and control of structural dynamics using recursive lattice filters
- Adaptive wall wind tunnels : a selected, annotated bibliography
- Adhesion between polymers and evaporated gold and nickel films
- Advanced fabrication techniques for hydrogen-cooled engine structures : [final report]
- Advances in planetary geology
- Advances in planetary geology
- Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices
- Aeroacoustic research facilities at NASA Langley Research Center : description and operational characteristics
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic characteristics at low Reynolds numbers of several heat-exchanger configurations for wind-tunnel use
- Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement
- Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic characteristics of a series of bodies with variations in nose camber
- Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations
- Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations
- Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic characteristics of wheelchairs
- Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept
- Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory
- Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment
- Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine
- Aerodynamic force measurements with a strain-gage balance in a cryogenic wind tunnel
- Aerodynamic heating on the corrugated surface of a 10.20 half-angle blunted cone at Mach 6.7
- Aerodynamic interactions from reaction controls for lateral control of the M2-F2 lifting-body entry configuration at transonic and supersonic mach numbers
- Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage
- Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles
- Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
- Aeronautical engineering
- Aeropropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
- Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
- Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20
- Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings
- Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards
- Aerospace medicine and biology
- Aerospace medicine and biology
- Aerospace medicine and biology
- Aerothermal analysis of a wing-elevon cove with variable leakage
- Aerothermal analysis of a wing-elevon cove with variable leakage
- Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
- Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
- Aerothermal performance and damage tolerance of a René 41 metallic standoff thermal protection system at mach 6.7
- Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6
- Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
- Airborne measurements of launch vehicle effluent : launch of space shuttle (STS-1) on April 12, 1981
- Airborne measurements of launch vehicle effluent of STS-2 launch on November 12, 1981, at Cape Canaveral, Florida
- Aircraft noise prediction program : theoretical manual
- Aircraft noise prediction program user's manual
- Aircrew displays and avionics for application in a future national airspace system
- Airfoil interaction with an impinging vortex
- Airport noise impact reduction through operations
- Algorithm for astronomical extended source, signal-to-noise ratio calculations
- Algorithm for astronomical, point source, signal to noise ratio calculations
- Algorithm for fixed-range optimal trajectories
- Algorithm for fixed-range optimal trajectories
- Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction
- An Algorithm for maximum likelihood estimation using an efficient method for approximating sensitivities
- An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations
- An Operational evaluation of head-up-displays for civil transport operations : NASA/FAA phase III final report
- An abrasion-ablation model description of galactic heavy-ion fragmentation
- An advanced cockpit instrumentation system : the coordinated cockpit display
- An aerodynamic analysis computer program and design notes for low speed wing flap systems
- An airport wind shear detection and warning system using Doppler radar : a feasibility study
- An algorithm for minimum-cost set-point ordering in a cryogenic wind tunnel
- An analytical study of the longitudinal response of airplanes to positive wind shear
- An analytical technique for approximating unsteady aerodynamics in the time domain
- An analytical technique for approximating unsteady aerodynamics in the time domain
- An application of multivariable design techniques to the control of the National Transonic Facility
- An approximate analytical method for vortex-lift and center of pressure on the slender wing
- An assessment of the capability to calculate tilting prop-rotor aircraft performance, loads, and stability
- An asymptotic expansion approach to the inverse radiative transfer problem
- An efficient algorithm for generating random number pairs drawn from a bivariate normal distribution
- An electrochemical method for determining hydrogen concentrations in metals and some applications
- An evaluation of superminicomputers for thermal analysis
- An evaluation of the NASA Tech House, including live-in test results
- An exact solution for the solidification of a liquid slab of binary mixture
- An experimental and theoretical investigation of deposition patterns from an agricultural airplane
- An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics
- An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect
- An experimental evaluation of head-up display formats / J.M. Naish and Donna L. Miller
- An exploratory investigation of the effect of a plastic coating on the profile drag of a practical-metal-construction sailplane airfoil
- An improved transverse shear deformation theory for laminated anisotropic plates
- An overview of artificial intelligence and robotics
- An overview of artificial intelligence and robotics, Volume I | Part A, Artificial intelligence | The core ingredients
- Analyses of surface cracks in finite plates under tension or bending loads
- Analysis and Monte Carlo simulation of near-terminal aircraft flight paths
- Analysis and simulation of a magnetic bearing suspension system for a laboratory model annular momentum control device
- Analysis of a MIL-L 27502 lubricant from a gas-turbine engine test by a size-exclusion chromatography
- Analysis of a topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel
- Analysis of aerodynamic coefficients using gust gradient data : spanwise turbulence effects on airplane response
- Analysis of airborne doppler lidar, doppler radar, and tall tower measurements of atmospheric flows in quiescent and stormy weather
- Analysis of costs of gallium arsenide and silicon solar arrays for space power applications
- Analysis of effect of flameholder characteristics on lean, premixed, partially vaporized fuel-air mixture quality and nitrogen oxides emissions
- Analysis of gap heating due to stepped tiles in the shuttle thermal protection system
- Analysis of jimsphere pairs for use in assessing space vehicle ascent capability
- Analysis of large space structures assembly : man/machine assembly analysis
- Analysis of noise measured from a propeller in a wake
- Analysis of normalized radar cross section ( ) signature of Amazon rain forest using Seasat scatterometer data
- Analysis of oscillatory motion of a light airplane at high values of lift coefficient
- Analysis of potential benefits of integrated-gasifier combined cycles for a utility system
- Analysis of random signal combinations for spacecraft pointing stability
- Analysis of rectangular microstrip antennas
- Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel
- Analysis of thermoelectric properties of high-temperature complex alloys of nickel-base, iron-base, and cobalt-base groups
- Analytic investigation of effect of end-wall contouring on stator performance
- Analytic model for washout of HCl (g) from dispersing rocket exhaust clouds
- Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
- Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
- Analytical investigation of synchrophasing as a means of reducing aircraft interior noise
- Analytical prediction and experimental verification of performance, at various operating conditions, of a dual-mode traveling wave tube with multistage depressed collectors
- Analytical study of acoustic response of a semireverberant enclosure with application to active noise control
- Analytical study of acoustic response of a semireverberant enclosure with application to active noise control
- Anisotropic friction, deformation, and fracture of single-crystal silicon carbide at room temperature
- Annealing of radiation damage in 0.1- and 2-ohm-centimeter silicon solar cells / Irving Weinberg and Clifford K. Swartz
- Annoyance caused by propeller airplane flyover noise
- Annoyance due to multiple airplane noise exposure
- Annual report
- Antarctic field tests of SARSAT personal locater beacons
- Application guide for universal source encoding for space
- Application of Zimmerman flutter-margin criterion to a wind-tunnel model
- Application of a Gaussian multilayer diffusion model to characterize dispersion of vertical HCL column density in rocket exhaust clouds
- Application of a computerized vibroacoustic data bank for random vibration criteria development
- Application of a numerical orthogonal coordinate generator to axisymmetric blunt bodies
- Application of a performance modeling technique to an airplane with variable sweep wings
- Application of information theory to the design of line-scan imaging systems
- Application of model control to wing-flutter suppression
- Application of modified profile analysis to function testing of simulated CTOL transport touchdown-performance data
- Application of modified profile analysis to function testing of the motion/no-motion issue in an aircraft ground-handling simulation
- Application of queueing models to multiprogrammed computer systems operating in a time-critical environment
- Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
- Applications systems verification and transfer project
- Approaches toward a blue semiconductor laser
- Approaches toward a blue semiconductor laser
- Approximate analysis of thermal convention in a crystal-growth cell for spacelab 3
- Approximation methods for combined thermal/structural design
- Archival of Seasat-A satellite scatterometer data merged with in situ data at selected, illuminated sites over the ocean
- Archival of aircrart scatterometer data from AAFE RADSCAT mission
- Assessment of ground effects on the propagation of aircraft noise : the T-38A flight experiment
- Astronautics and aeronautics
- Astronautics and aeronautics
- Atlas of Comet Halley 1910 II
- Atmospheric constraint statistics for the space shuttle mission planning
- Atmospheric simulator and calibration system for remote sensing radiometers
- Atmospheric solar absorption measurements in the 9 to 11 [mu]m region using a diode laser heterodyne spectrometer
- Atmospheric solar absorption measurements in the 9 to 11 um region using a diode laser heterodyne spectrometer
- Auger spectroscopy analysis of lubrication with zinc dialkyldithiophosphate of several metal combinations in sliding contact
- Automated optimum design of wing structures : deterministic and probabilistic approaches
- Automated procedure for developing hybrid computer simulations of turbofan engines
- Automatic rendezvous and docking : a parametric study
- Avenues and incentives for commercial use of a low-gravity environment
- Axial jet mixing of ethanol in cylindrical containers during weightlessness
- Beam impingement angle effects on secondary electron emission characteristics of textured pyrolytic graphite
- Beaufort/Bering 1979 microwave remote sensing data catalog report-March 14-24, 1979
- Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : a slip-velocity-controlled, pressure-bias-modulated system
- Behavior of aircraft antiskid braking systems on dry and wet runway surfaces : hydromechanically controlled system
- Bending stiffness of multiwall sandwich
- Beyond the atmosphere : early years of space science
- Body and canard effects on an attached-flow maneuver wing at Mach 1.62
- Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50
- Bubble Memory Module
- Buckling and failure characteristics of graphite-polyimide shear panels
- Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder
- Calculation of composition distribution of ultrafine ion-H2O-H2SO4 clusters using a modified binary ion-nucleation theory
- Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
- Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
- Calculation of three-dimensional unsteady transonic flows past helicopter blades
- Calculation of three-dimensional unsteady transonic flows past helicopter blades
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data
- Calibration of sonic valves for the laminar flow control, leading-edge flight test
- Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams
- Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams
- Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle
- Capturing energy from the wind
- Carbon monoxide measurement in the Global Atmospheric Sampling Program
- Carbon-catalyzed oxidation of SO2 by NO2 and air
- Case studies of clear air turbulence using the Diagnostic Richardson Number Tendency formulation
- Catalog of Earth photographs from the Apollo-Soyuz test project
- Cavitation pitting and erosion of aluminum 6061-T6 in mineral oil and water
- Changes in surface chemistry of silicon carbide (0001) surface with temperature and their effect on friction
- Characteristic vector analysis of inflection ratio spectra : new technique for analysis of ocean color data
- Characterization of erosion of metallic materials under cavitation attack in a mineral oil
- Characterization of large 2219 aluminum alloy hand forgings for the space shuttle solid rocket booster / M.W. Brennecke
- Characterization of noncontact piezoelectric transducer with conically shaped piezoelement
- Characterization of soil and postlaunch pad debris from Cape Canaveral launch complex and analysis of soil interaction with aqueous HCl
- Chariots for Apollo : a history of manned lunar spacecraft
- Charts for determing potential minimum sonic-boom overpressures for supersonic cruise aircraft
- Chemical kinetic analysis of hydrogen-air ignition and reaction times
- Chemical kinetic models for combustion of hydrocarbons and formation of nitric oxide
- Chemical kinetic models for combustion of hydrocarbons and formation of nitric oxide
- Chemical mechanisms and reaction rates for the initiation of hot corrosion of IN-738
- Circuit transients due to negative bias arcs on a high-voltage solar array in low earth orbit
- Circumferentially segmented duct liners optimized for axisymmetric and standing-wave sources
- Cloud-encounter and particle-concentration variabilities from GASP data
- Cognitive issues in head-up displays
- Cognitive issues in head-up displays
- Coherent large-scale structures in high Reynolds number supersonic jets
- Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66
- Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66
- Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine
- Colorimetric principles as applied to multichannel imagery
- Combined single-pulse holography and time-resolved laser schlieren for flow visualization
- Combustion gas properties : I-ASTM jet A fuel and dry air
- Comparative analyses of space-to-space central power stations
- Comparative analysis of PA-1-350 chieftain (N44LV) accident and NASA crash test data
- Comparative performance of HgCdTe photodiodes for heterodyne application
- Comparative performance of HgCdTe photodiodes for heterodyne application
- Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests
- Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls
- Comparison of analytical predictions of longitudinal short-period pilot-induced oscillations with results from a simulation study of the space shuttle orbiter
- Comparison of data inversion techniques for remotely sensed wide-angle observations of earth emitted radiation
- Comparison of experimental and theoretical turbulence reduction characteristics for screens, honeycomb, and honeycomb-screen combinations
- Comparison of low-altitude wind-shear statistics derived from measured and proposed standard wind profiles
- Comparison of measured and calculated mode redistribution associated with spinning mode transmission through circumferentially segmented lined ducts
- Comparison of multispectral remote-sensing techniques for monitoring subsurface drain conditions
- Comparison of numerical techniques for integration of stiff ordinary differential equations arising in combustion chemistry
- Comparison of predicted and experimental thermal performance of angular-contact ball bearings
- Comparison of predicted and measured elastohydrodynamic film thickness in a 20-millimeter-bore ball bearing
- Comparison of simulator fidelity model predictions with in-simulator evaluation data
- Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests
- Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels
- Comparison of three thrust calculation methods using in-flight thrust data
- Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor
- Comparisons of modified VASCO X-2 and AISI 9310 gear steels
- Compression failure mechanisms of composite structures
- Computational methods for analyzing the transmission characteristics of a Beta Particle magnetic analysis system
- Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel
- Computer code for off-design performance analysis of radial-inflow turbines with rotor blade sweep
- Computer modeling of multiple-channel input signals and intermodulation losses caused by nonlinear traveling-wave-tube amplifiers
- Computer program for aerodynamic and blading design of multistage axial-flow compressors
- Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row
- Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade
- Computer program for pulsed thermocouples with corrections for radiation effects
- Computer program for solving laminar, transitional, or turbulent compressible boundary-layer equations for two-dimensional and axisymmetric flow
- Computer program to predict aircraft noise levels
- Computer simulation of random variables and vectors with arbitrary probability distribution laws
- Computer-automated opponent for manned air-to-air combat simulations
- Computer-automated opponent for manned air-to-air combat simulations
- Concept for a power system controller for large space electrical power systems
- Conceptual model of turbulent flameholding for scramjet combustors
- Conceptual model of turbulent flameholding for scramjet combustors
- Conceptual study of a turbojet/ramjet inlet
- Concurrent error-detecting codes for arithmetic processors
- Conference papers
- Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft
- Considerations for the installation of honeycomb and screens to reduce wind-tunnel turbulence
- Contoured tank outlets for draining of cylindrical tanks in low-gravity environment
- Contracts, grants, and funding summary of supersonic cruise research and variable-cycle engine technology programs : 1972-1982
- Cornering characteristics of the nose-gear tire of the Space Shuttle Orbiter
- Correlation and assessment of structural airplane crash data with flight parameters at impact
- Correlation of asperity contact-time fraction with elastohydrodynamic film thickness in a 20-millimeter-bore ball bearing
- Correlation of asperity contact-time fraction with elastohydrodynamic film thickness in a 20-millimeter-bore ball bearing
- Correlation of ideal and actual shear strengths of metals with their friction properties
- Correlation of predicted and measured sonic boom characteristics from the reentry of STS-1 Orbiter
- Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise
- Coupled wave model for large magnet coils
- Crash tests of four low-wing twin-engine airplanes with truss-reinforced fuselage structure
- Crash tests of three identical low-wing single-engine airplanes
- Creep and residual mechanical properties of cast superalloys and oxide dispersion stengthened alloys
- Criteria for self-ignition of supersonic hydrogen-air mixtures
- Crossflow effects on steady and fluctuating pressures on an ogive-cylinder cone-frustum model in supersonic separated flow