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Multibody interference at transonic Mach numbersAn experimental and computational study has been made of the forces and moments on multibody configurations at Mach numbers from 0.6 to 1.2. The interference forces and moments that occur on symmetric double and triple body configurations at zero angle of attack are examined in detail. In all cases, the normal interference force is always in a direction to pull the bodies together and the moment about the 0.5L point is always to rotate the tips of the bodies away from the center of the configuration. The axial interference force (pressure drag at zero angle of attack) increases the drag per store as additional stores are added to the configuration. The effect of angle of attack on the interference is relatively small.
Document ID
19920044399
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chapman, Gary T.
(NASA Ames Research Center Moffett Field, CA, United States)
Bonness, William K.
(California, University Berkeley, United States)
Lynch, Prisca L.
(USAF, Armament Directorate, Eglin AFB FL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-0651
Accession Number
92A27023
Funding Number(s)
CONTRACT_GRANT: NCA2-529
Distribution Limits
Public
Copyright
Other

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