3 edition of Flight-determined benefits of integrated flight-propulsion control systems found in the catalog.
Flight-determined benefits of integrated flight-propulsion control systems
by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va
Written in English
|Other titles||Flight determined benefits of integrated flight ....|
|Statement||James F. Stewart, Frank W. Burcham, Jr., and Donald H. Gatlin.|
|Series||NASA technical memorandum -- 4393.|
|Contributions||Burcham, Frank W., Gatlin, Donald H., United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.|
|The Physical Object|
mil-hdbk(mi) 4. Chapter 5, Aerodynamics, presents design curves, equations, and data that will permit the prediction of stability and drag characteristics for commonly used aerodynamic bodies or combinations of bodies, including various types of fins and other stabilizing devices. here - Private Data LLC. READ.
The past decade has seen a return to hypersonic flight with the record setting Mach 7 and Mach 10 flights of the XA, successful flight testing of neural nets integrated into flight control systems, flight testing to understand and mitigate sonic booms, the return of wing warping for aerodynamic control, and an increase in flight activity of.  James F. Stewart, Frank W. Burcham, Jr., Donald H. Gatlin, “Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems,” NASA Technical Memorandum , June,  Sarah L. Gatley, Declan G. Bates, Ian Postlethwaite, “A Partitioned Integrated Flight and Propulsion Control System with Engine Safety Limiting.
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SyntaxTextGen not activatedRichard Whitcomb and the Quest for Aerodynamic Efficiency Pdf and the Rotary Wing Revolution Softening the Sonic Boom: 50 Years of NASA Research Toward Transatmospheric Fl.main NASAsContributionsToAeronauticsVolume1-eBook 2 - Free ebook download as PDF File .pdf), Text File .txt) or read book online for free.The main areas under investigation included inlet design analysis, propul- sion system steady-state and ebook performance, inlet engine control systems, and airframe/propulsion interactions.
Engineers and scientists from NASA Ames, NASA Langley, NASA Lewis, and the NASA FRC all contributed to the YF propulsion studies.