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Fixed base simulator study of an externally blown flap STOL transport airplane during approach and landingA fixed-base simulator study was conducted to determine the flight characteristics of a representative STOL transport having a high wing and equipped with an external-flow jet flap in combination with four high-bypass-ratio fan-jet engines during the approach and landing. Real-time digital simulation techniques were used. The computer was programed with equations of motion for six degrees of freedom and the aerodynamic inputs were based on measured wind-tunnel data. A visual display of a STOL airport was provided for simulation of the flare and touchdown characteristics. The primary piloting task was an instrument approach to a breakout at a 200-ft ceiling with a visual landing.
Document ID
19720025380
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Grantham, W. D.
(NASA Langley Research Center Hampton, VA, United States)
Nguyen, L. T.
(NASA Langley Research Center Hampton, VA, United States)
Patton, J. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Deal, P. L.
(NASA Langley Research Center Hampton, VA, United States)
Champine, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Carter, C. R.
(Army Air Mobility R and D Lab.)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6898
L-8394
Report Number: NASA-TN-D-6898
Report Number: L-8394
Accession Number
72N33030
Funding Number(s)
PROJECT: RTOP 760-61-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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