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A review of recent developments in flight test techniques at the Ames Research Center, Dryden Flight Research FacilityNew flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination with ground and airborne computational capabilities to maximize data return is discussed, including the remotely piloted research vehicle technique for high-risk testing, the remotely augmented vehicle technique for handling qualities research, and use of ground computed flight director information to fly unique profiles such as constant Reynolds number profiles through the transonic flight regime. Techniques used for checkout and design verification of systems-oriented aircraft are discussed, including descriptions of the various simulations, iron bird setups, and vehicle tests. Some newly developed techniques to support the aeronautical research disciplines are discussed, including a new approach to position-error determination, and the use of a large skin friction balance for the measurement of drag caused by various excrescencies.
Document ID
19840012447
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Layton, G. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1237
NAS 1.15:86039
NASA-TM-86039
Report Number: H-1237
Report Number: NAS 1.15:86039
Report Number: NASA-TM-86039
Meeting Information
Meeting: Canadian Aeronautics and Space Inst. (CASI) Flight Test Symp.
Location: Cold Lake, Alberta
Country: Canada
Start Date: April 11, 1984
End Date: April 12, 1984
Accession Number
84N20515
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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