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NASA general aviation technology programsThis paper describes the status of the current NASA programs that are aimed at providing new technology for aircraft designs that will improve both safety and utility while reducing the environmental impact of general aviation to acceptable levels. Safety related areas that are discussed include the full scale crash test program and the stall/spin research effort. Among the programs addressing increased utility and performance, advanced airfoil developments and engine cooling drag reduction are discussed. Noise and emission reduction is a subject that is receiving significant emphasis within the NASA programs. Also included is a description of the current status of the hydrogen injection concept as a means of both lowering emissions and increasing fuel economy.
Document ID
19750040935
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Winblade, R. L.
(NASA General Aviation Technology Office Washington, D.C., United States)
Date Acquired
August 8, 2013
Publication Date
February 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 75-290
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Annual Meeting and Technical Display
Location: Washington, DC
Start Date: February 24, 1975
End Date: February 26, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A25007
Distribution Limits
Public
Copyright
Other

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