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Dynamic wind tunnel testing techniques.Dynamic wind tunnel testing techniques and program of advanced analysis of full-scale free- flight missile performance data
Document ID
19660062038
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Eikenberry, R. S.
Nicolaides, J. D.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 66-752
Report Number: AIAA PAPER 66-752
Accession Number
66A41328
Funding Number(s)
CONTRACT_GRANT: AF 08/635/-5275
CONTRACT_GRANT: NSR-15-004-016
CONTRACT_GRANT: PO-28-017-A6-08594/A/
CONTRACT_GRANT: DA-18-035-AMC-356/A/
Distribution Limits
Public
Copyright
Other
Keywords
MISSILE TEST
WIND TUNNEL STABILITY TEST

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