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A STOL airworthiness investigation using a simulation of an augmentor wing transport. Volume 2: Simulation data and analysisA simulator study of STOL airworthiness was conducted using a model of an augmentor wing transport. The approach, flare and landing, go-around, and takeoff phases of flight were investigated. The simulation and the data obtained are described. These data include performance measures, pilot commentary, and pilot ratings. A pilot/vehicle analysis of glide slope tracking and of the flare maneuver is included.
Document ID
19750017845
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Heffley, R. K. (NASA Ames Research Center Moffett Field, CA, United States)
Stapleford, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Rumold, R. C. (NASA Ames Research Center Moffett Field, CA, United States)
Lehman, J. M. (NASA Ames Research Center Moffett Field, CA, United States)
Scott, B. C. (NASA Ames Research Center Moffett Field, CA, United States)
Hynes, C. S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-5798
FAA-RD-74-179-VOL-2
AD-A006602
NASA-TM-X-62396
Report Number: A-5798
Report Number: FAA-RD-74-179-VOL-2
Report Number: AD-A006602
Report Number: NASA-TM-X-62396
Accession Number
75N25917
Funding Number(s)
CONTRACT_GRANT: NAS2-7926
PROJECT: RTOP 182-530-035-2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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