#
Aeroelasticity
Resource Information
The concept ** Aeroelasticity** represents the subject, aboutness, idea or notion of resources found in **Missouri University of Science & Technology Library**.

The Resource
Aeroelasticity
Resource Information

The concept

**Aeroelasticity**represents the subject, aboutness, idea or notion of resources found in**Missouri University of Science & Technology Library**.- Label
- Aeroelasticity

- Source
- nasat

## Context

Context of Aeroelasticity#### Subject of

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- Wing-body aeroelasticity on parallel computers
- A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development
- A numerical model of unsteady, subsonic aeroelastic behavior
- A worst-case approach for on-line flutter prediction
- ASTROP2 users manual : a program for aeroelastic stability analysis of propfans
- ASTROP2 users manual : a program for aeroelastic stability analysis of propfans
- Advanced technology subsonic transport study : N+3 technologies and design concepts
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aeroelastic analyses of the SemiSpan Supersonic Transport (S4T) wind tunnel model at Mach 0.95
- Aeroelastic computations of a compressor stage using the harmonic balance method
- Aeroelastic deformation : adaptation of wind tunnel measurement concepts to full-scale vehicle flight testing
- Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
- Aeroelastic stability and response of rotating structures : final technical report
- Aeroelastic stability computations for turbomachinery
- Aeroelastic stability computations for turbomachinery
- Aeroelastic stability of a full-scale hingeless rotor
- Aeroelastic tailoring of transport aircraft wings : state-of-the-art and potential enabling technologies
- Aeroelastic tailoring via tow steered composites
- Aircraft structural mass property prediction using conceptual-level structural analysis
- Airloads, wakes, and aeroelasticity
- Algorithm for simulating atmospheric turbulence and aeroelastic effects on simulator motion systems
- An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
- An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
- An aeroelastician's perspective of wind tunnel and flight experiences with active control of structural response and stability
- An analytical technique for approximating unsteady aerodynamics in the time domain
- An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
- An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence
- Analytical flutter investigation of a composite propfan model
- Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers
- Application of the ASP3D computer program to unsteady aerodynamic and aeroelastic analyses
- Artificial intelligence based control power optimization on tailless aircraft : ARMD seedling fund, phase I, final report
- Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods
- Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study
- Comprehensive modeling and analysis of rotorcraft variable speed propulsion system with coupled engine/transmission/rotor dynamics
- Computational engine structural analysis
- Design and fabrication of the NASA decoupler pylon for the F-16 aircraft
- Development and testing of control laws for the active aeroelastic wing program
- Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D
- Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan
- Experimental aeroelasticity history, status and future in brief
- Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft
- Exploratory studies in generalized predictive control for active aeroelastic control of tiltrotor aircraft
- Factorization and reduction methods for optimal control of distributed parameter systems
- Final technical report for aeroelastic analysis of turbomachinery for space propulsion : NASA grant number NAG3-1449, grant duration--January 13, 1993 to February 23, 1996
- Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
- Flutter analysis of a transonic fan
- Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
- Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
- Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept
- Harmonic balance computations of fan aeroelastic stability
- Identification of XV-15 aeroelastic modes using frequency-domain methods
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Improving CPA-TSD steady pressure solutions through airfoil slope modification
- Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Introduction of the ASP3D computer program for unsteady aerodynamic and aeroelastic analyses
- Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
- Machine dynamics branch research and accomplishments for FY 1996
- Material and thickness grading for aeroelastic tailoring of the common research model wing box
- Method for experimental determination of flutter speed by parameter identification
- Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment
- Nonlinear dynamic modeling and controls development for supersonic propulsion system research
- Nonstationary dynamics data analysis with wavelet-SVD filtering
- Novel control effectors for truss braced wing
- Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter
- Prediction of wing aeroelastic effects on aircraft lift and pitching moment characteristics
- Quiet High Speed Fan II (QHSF II) : final report
- Re-computation of numerical results contained in NACA report no. 496
- Research and applications in structures at the NASA Langley Research Center
- Robust flutter margin analysis that incorporates flight data
- Rotating shake test and modal analysis of a model helicopter rotor blade
- Rotating shake test and modal analysis of a model helicopter rotor blade
- Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Static aeroelastic analysis of a three-dimensional generic wing
- Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990
- TURBOMAT : a probabilistic turbomachinery aeroelastic analysis tool
- The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel
- The sound of moving bodies
- Tiltrotor vibration reduction through higher harmonic control
- Unsteady aerodynamic model tuning for precise flutter prediction
- Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
- Validation of design and analysis techniques of tailored composite structures
- Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) Program
- Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program
- Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data
- Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data

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