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VTOL in ground effect flows for closely spaced jetsResults of a series of in ground effect twin jet tests are presented along with flow models for closely spaced jets to help predict pressure and upwash forces on simulated aircraft surfaces. The isolated twin jet tests revealed unstable fountains over a range of spacings and jet heights, regions of below ambient pressure on the ground, and negative pressure differential in the upwash flow field. A separate computer code was developed for vertically oriented, incompressible jets. This model more accurately reflects fountain behavior without fully formed wall jets, and adequately predicts ground isobars, upwash dynamic pressure decay, and fountain lift force variation with height above ground.
Document ID
19810010569
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Migdal, D.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Hill, W. G., Jr.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Jenkins, R. C.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-152321
Report Number: NASA-CR-152321
Accession Number
81N19095
Funding Number(s)
CONTRACT_GRANT: NAS2-10097
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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