NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Recommendations for ground effects research for V/STOL and STOL aircraft and associated equipment for large scale testingThe current understanding of the effects of ground proximity on V/STOL and STOL aircraft is reviewd. Areas covered include (1) single jet suckdown in hover, (2) fountain effects on multijet configurations, (3) STOL ground effects including the effect of the ground vortex flow field, (4) downwash at the tail, and (5) hot gas ingestion in both hover and STOL operation. The equipment needed for large scale testing to extend the state of the art is reviewed and developments in three areas are recommended as follows: (1) improve methods for simulating the engine exhaust and inlet flows; (2) develop a model support system that can simulate realistic rates of climb and descent as well as steady height operation; and (3) develop a blowing BLC ground board as an alternative to a moving belt ground board to properly simulate the flow on the ground.
Document ID
19880008201
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuhn, Richard E.
(Kuhn (Richard E.) Newport News, VA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-177429
NAS 1.26:177429
Report Number: NASA-CR-177429
Report Number: NAS 1.26:177429
Accession Number
88N17585
Funding Number(s)
PROJECT: RTOP 505-43-01
CONTRACT_GRANT: NAS2-11912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available