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Integration of a mechanical forebody vortex control system into the F-15The goal of the F-15 Forebody Vortex Control (FVC) program is to develop a production FVC system for the F-15. The system may consist of either a mechanically actuated device such as the strakes developed for the HARV program, or a pneumatic device such as the port blowing system being tested on the X-29. Both types of systems are being evaluated under this program. Background information on the F-15 and a description and overview of forebody vortex controls (FVC) will be presented.
Document ID
19950007844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boalbey, Richard E.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Citurs, Kevin D.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Ely, Wayne L.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Harbaugh, Stephen P.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Hollingsworth, William B.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Phillips, Ronald L.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: NASA. Dryden Flight Research Center, Fourth High Alpha Conference, Volume 3
Subject Category
Aerodynamics
Accession Number
95N14258
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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