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Fin loads and control-surface hinge moments measured in full-scale wind-tunnel tests on the X-24A flight vehicleFin loads and control surface hinge moments measured in full scale wind tunnel tests on X-24A flight vehicle
Document ID
19710005026
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
De Angelis, V. M. (NASA Flight Research Center Edwards, CA, United States)
Tang, M. H. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1922
H-580
Report Number: NASA-TM-X-1922
Report Number: H-580
Accession Number
71N14501
Funding Number(s)
CONTRACT_GRANT: 727-00-00-01-24
Distribution Limits
Public
Copyright
Other

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