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Advanced prediction technique for the low speed aerodynamics of V/STOL aircraft. Volume 1: Technical discussionThe V/STOL Aircraft Propulsive Effects (VAPE) computerized prediction method is evaluated. The program analyzes viscous effects, various jet, inlet, and Short TakeOff and Landing (STOL) models, and examines the aerodynamic configurations of V/STOL aircraft.
Document ID
19840018594
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Beatty, T. D. (Vought Corp. Dallas, TX, United States)
Worthey, M. K. (Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
March 15, 1984
Subject Category
Aerodynamics
Report/Patent Number
REPT-2-55110/3R-53463-VOL-1
NAS 1.26:166442-VOL-1
NASA-CR-166442-VOL-1
Report Number: REPT-2-55110/3R-53463-VOL-1
Report Number: NAS 1.26:166442-VOL-1
Report Number: NASA-CR-166442-VOL-1
Accession Number
84N26662
Funding Number(s)
PROJECT: RTOP 505-43-01
CONTRACT_GRANT: NAS2-11156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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