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The present status and the future of missile aerodynamicsRecent developments in the state of the art in missile aerodynamics are reviewed. Among the subjects covered are: (1) Tri-service/NASA data base, (2) wing-body interference, (3) nonlinear controls, (4) hypersonic transition, (5) vortex interference, (6) airbreathers, supersonic inlets, (7) store separation problems, (8) correlation of missile data, (9) CFD codes for complete configurations, (10) engineering prediction methods, and (11) future configurations. Suggestions are made for future research and development to advance the state of the art of missile aerodynamics.
Document ID
19900000735
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nielsen, Jack N. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1989
Publication Information
Publication: AGARD, Stability and Control of Tactical Missile Systems
Subject Category
Aerodynamics
Accession Number
90N10051
Distribution Limits
Public
Copyright
Other
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