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Filament wound data base development, revision 1, appendix BThe data tape 8 data are presented in tabular form. Each page consists of six-component force and moment coefficients as they vary with angle of attack at a specific Mach number and roll angle. The angle of attack range is from 0 to 180 deg in 5 deg increments. The six coefficients are normal force, pitching moment, side force, yawing moment, axial force, and rolling moment. Each successive page is incremented for roll angle in 45 deg increments for a roll angle range from 0 to 360 deg. The cycle is then repeated for the next Mach number. The Mach numbers in the data base are 0.4, 0.5, 0.55, 0.6, 0.7, 0.8, 0.9, 0.95, 1.05, 1.1, 1.2, 1.4, 1.96, 2.5, 3.0, and 3.48.
Document ID
19870011584
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sharp, R. Scott
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Braddock, William F.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-179070
NAS 1.26:179070
LMSC-HREC-TR-D951500-1B
Report Number: NASA-CR-179070
Report Number: NAS 1.26:179070
Report Number: LMSC-HREC-TR-D951500-1B
Accession Number
87N21017
Funding Number(s)
CONTRACT_GRANT: NAS8-35054
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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