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V/STOL aircraft and fluid dynamicsThe impact of military applications on rotorcraft and V/STOL aircraft design is summarized with respect to fixed-wing aircraft. The influence of the mission needs on the configurational design of V/STOL aircraft, the implications regarding some problems in fluid dynamics relating to propulsive flows, and their interaction with the aircraft and the ground plane, are also considered. Additional research in fluid dynamics that can contribute to an improvement in performance of V/STOL aircraft is suggested.
Document ID
19820002156
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Roberts, L. (Stanford Univ. Calif., United States)
Anderson, S. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81328
A-8730
Report Number: NASA-TM-81328
Report Number: A-8730
Accession Number
82N10029
Funding Number(s)
PROJECT: RTOP 505-42-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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