Aircraft engines
Resource Information
The concept Aircraft engines represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
The Resource
Aircraft engines
Resource Information
The concept Aircraft engines represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
- Label
- Aircraft engines
- Source
- nasat
85 Items that share the Concept Aircraft engines
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- Validation of an integrated airframe and turbofan engine simulation for evaluation of propulsion control modes
- A modular framework for modeling hardware elements in distributed engine control systems
- A multidisciplinary approach to mixer-ejector analysis and design
- A sensitivity study of commercial aircraft engine response for emergency situations
- A systematic approach to sensor selection for aircraft engine health estimation
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- Acoustic directivity and insertion loss measurements of advanced liners installed in the inlet of the DGEN aeropropulsion research turbofan
- Advanced seal technology role in meeting next generation turbine engine goals
- Aeropropulsion facilities configuration control : procedures manual
- Air Force F-16 aircraft engine aerosol emissions under cruise altitude conditions
- Aircraft engine gas path diagnostic methods : public benchmarking results
- Aircraft engine technology for green aviation to reduce fuel burn
- Aircraft turbine engine control research at NASA Glenn Research Center
- An air-breathing launch vehicle concept for single-stage-to-orbit
- An analytical assessment of NASA's N+1 Subsonic Fixed Wing Project noise goal
- Analytical fuel property effects : final report, Phase 2, Small combustors
- Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters
- Application of computational fluid dynamics in high speed aeropropulsion
- Artificial neural networks applications : from aircraft design optimization to orbiting spacecraft on-board environment monitoring
- Artificial neural networks applications : from aircraft design optimization to orbiting spacecraft on-board environment monitoring
- Attachment of lead wires to thin film thermocouples mounted on high temperature materials using the parallel gap welding process
- Benchmarking model variants in development of a hardware-in-the loop simulation system
- Cascade optimization strategy for aircraft and air-breathing propulsion system concepts
- Cascade optimization strategy for aircraft and air-breathing propulsion system concepts
- Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine
- Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine
- Control of flow separation and mixing by aerodynamic excitation
- Current Lewis turbomachinery research : building on our legacy of excellence
- Current status of post-combustor trace chemistry modeling and simulation at NASA Glenn Research Center
- Deformation mechanisms of NiAl cyclicly deformed near the brittle-to-ductile transition temperature : final report
- Design and development of an F/A-18 inlet distortion rake : a cost and time saving solution
- Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine
- Development of a twin-spool turbofan engine simulation using the toolbox for the modeling and analysis of thermodynamic systems (T-MATS)
- Development of optical diaphragm deflection sensors : final report
- Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance
- Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane
- Elevated temperature crack growth : final report
- Engine icing modeling and simulation (Part 2) : performance simulation of engine rollback phenomena, Part 2
- Experimental characterization of gas turbine emissions at simulated flight altitude conditions : final report for period January 1995 to April 1996
- Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design
- Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design
- Future fuel scenarios and their potential impact to aviation
- General aviation light aircraft propulsion : from the 1940's to the next century
- General aviation light aircraft propulsion : from the 1940's to the next century
- HBCUs/OMUs Research Conference agenda and abstracts : proceedings of a conference held at Ohio Aerospace Institute and sponsored by NASA Glenn Research Center, Cleveland, Ohio, April 17-18, 2001
- HBCUs/OMUs Research Conference agenda and abstracts : proceedings of a conference held at Ohio Aerospace Institute and sponsored by NASA Glenn Research Center, Cleveland, Ohio, April 17-18, 2002
- HPT clearance control : intelligent engine systems : phase 1
- High Stability Engine Control (HISTEC) : flight demonstration results
- High pressure turbine test hardware detailed design report
- High stability engine control (HISTEC)
- High stability engine control (HISTEC)
- High stability engine control (HISTEC) : flight demonstration results
- High stability engine control (HISTEC) flight test results
- High stability engine control (HISTEC) flight test results
- High temperature lightweight self-healing ceramic composites for aircraft engine applications
- Implementation of an integrated on-board aircraft engine diagnostic architecture
- Implementation of enhanced propulsion control modes for emergency flight operation
- Joint US / Russia TU-144 engine ground tests
- Joint US/Russia TU-144 engine ground tests
- Kalman filtering with inequality constraints for turbofan engine health estimation
- Lightweight two-stroke cycle aircraft diesel engine technology enablement program : final report
- Low pressure turbine test hardware detailed design report
- Measurements of turbulent flow field in separate flow nozzles with enhanced mixing devices, test report
- Model-based engine control architecture with an extended Kalman filter
- NASA aeropropulsion research
- NASA and general aviation
- NASA/DoD aerospace knowledge diffusion research project : results of the phase 1 mail survey--propulsion and aircraft engine perspective, Report number 41, The technical communication practices of U.S. aerospace engineers and scientists
- NPSS on NASA's information power grid : using CORBA and Globus to coordinate multidisciplinary aeroscience applications
- Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements
- Preliminary development of an intelligent computer assistant for engine monitoring
- Preliminary evaluation of a turbine/rotary combustion compound engine for a subsonic transport
- Probabilistic analysis of aircraft gas turbine disk life and reliability
- Probabilistic analysis of aircraft gas turbine disk life and reliability
- Propulsion Diagnostic Method Evaluation Strategy (ProDiMES) user's guide
- Quench crack behavior of nickel-base disk superalloys
- Shock generation and control using DBD plasma actuators : SBIR phase I final report
- Simulation of aircraft engine blade-out structural dynamics
- Simulation of aircraft engine blade-out structural dynamics
- Structural tailoring of select fiber composite structures
- Study of advanced fuel system concepts for commercial aircraft and engines
- Temperature distribution in a composite of opaque and semitransparent spectral layers
- Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Turboelectric aircraft drive key performance parameters and functional requirements
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/15zHlFO0dek/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/15zHlFO0dek/">Aircraft engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/15zHlFO0dek/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/15zHlFO0dek/">Aircraft engines</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
