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NASA DFRC Practices for Prototype QualificationThis slide presentation reviews the practices that Dryden uses for qualification of the prototypes of aircraft. There are many views of aircraft that Dryden has worked with. Included is a discussion of basic considerations for strength, a listing of standards and references, a discussion of typical safety of flight approaches, a discussion of the prototype design, using the X-29A as an example, and requirements for new shapes (i.e., the DAST-ARW1 , F-8 Super Critical Wing, AFTI/F-111 MAW), new control laws (i.e., AAW F-18), new operating envelope (i.e., F-18 HARV), limited sope add-on or substitute structure (i.e., SR-71 LASRE, ECLIPSE, F-16XL SLFC), and extensively modified or replaced structure (i.e., SOFIA, B747SP). There is a listing of causes for the failure of the prototype.
Document ID
20100017738
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Lokos, William A.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 29, 2013
Publication Date
October 19, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-1071
Report Number: DFRC-1071
Meeting Information
Meeting: NATO Research and Techology Organization AVT-174 (Applied Vehicle Technology) Meeting
Location: Bonn
Country: Germany
Start Date: October 19, 2009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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