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A simulator investigation of the influence of engine response characteristics on the approach and landing for an externally blown flap aircraft. Part 2: Aerodynamic modelAn analysis of the influence of engine response characteristics on the approach and landing of an externally blown flap aircraft was conducted using flight simulator facilities. The configuration of the aerodynamic model is described. The aerodynamic characteristics as a function of angle of attack, thrust coefficient, and flap deflection are presented in tabular form and as graphs.
Document ID
19730017295
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ciffone, D. L. (NASA Ames Research Center Moffett Field, CA, United States)
Robinson, G. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62265(2)
Report Number: NASA-TM-X-62265(2)
Accession Number
73N26022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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