NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Methods of determining the Saturn I BUFFETING response from rigid model wind tunnel tests, volume ISaturn I buffeting response data determined from rigid model wind tunnel tests - aerodynamic stability and aeroelasticity
Document ID
19660014345
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Boone, J. R. (Chrysler Corp. Huntsville, AL, United States)
Mc Canless, G. F. (Chrysler Corp. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-74370
HSM-R114, VOL. I
Report Number: NASA-CR-74370
Report Number: HSM-R114, VOL. I
Accession Number
66N23634
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC STABILITY
WIND TUNNEL STABILITY TEST
AEROELASTICITY
BUFFETING
SATURN I LAUNCH VEHICLE

Related Records

There are no records associated with this record.
No Preview Available