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Hot gas ingestion: From model results to full scale engine testingAn overview is presented of a joint NASA Lewis McDonnell Aircraft Co. Hot Gas Ingestion (HGI) test program in NASA Lewis' 9 x 15 foot Low Speed Wind Tunnel (LSWT). Advanced short takeoff vertical landing (ASTOVL) aircraft capable of operating from remote sites, damaged runways, aircraft carriers and small air-capable ships are being pursued for deployment around the turn of the century. To achieve this goal, it is important that technologies critical to this unique class of aircraft be developed. One of the ASTOVL concepts, the vectored thrust, has as its critical technology item, the potential of hot gas ingestion (which occurs during vertical flight operation while in ground effect) as a key development issue. Recognizing this need, NASA Lewis Powered Lift Section and McAir have defined a cooperative program for testing in the Lewis 9 x 15 foot LSWT. This program is described in detail.
Document ID
19870014986
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johns, Albert L.
(NASA Lewis Research Center Cleveland, OH, United States)
Biesiadny, Thomas J.
(NASA Lewis Research Center Cleveland, OH, United States)
Pagel, L. L.
(McDonnell Aircraft Co. St. Louis, Mo., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Publication Information
Publication: NASA. Ames Research Center Proceedings of the 1985 NASA Ames Research Center's Ground-Effects Workshop
Subject Category
Aircraft Propulsion And Power
Accession Number
87N24419
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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