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New Concepts in Developing Flight Airworthiness Requirements

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Tuck, Dennis A., author.
Conference Name:
National Business Aircraft Meeting and Engineering Display (1972-03-15 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
The FAA Flight Test Branch is now actively engaged in several regulatory development programs using resources made available by NASA, FAA, USAF, and others in industry. These resources include advanced flight simulators, variable stability aircraft, and current aircraft. These tools are in use now to develop standards proposals for supersonic transports, V/STOL, transports, and general aviation aircraft.Critical control and stability parameters may now be explored by FAA flight standards pilots in concert with other government and industry experts to the extent and with fidelity never before possible. An example of this approach may be found in the latest issue of the "Tentative Airworthiness Standards for Supersonic Transports." The SST performance standards therein resulted from an investigation of several aircraft models in the NASA Ames Flight Simulator for Advanced Aircraft and a small delta-winged fighter loaned by the Air Force
Notes:
Vendor supplied data
Publisher Number:
720306
Access Restriction:
Restricted for use by site license

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