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Aerodynamic results of a separation test (CA20) conducted at the Boeing transonic wind tunnel using 0.030-scale models of the configuration 140A/B (modified) SSV orbiter (model no. 45-0) and the Boeing 747 carrier (model no. AX 1319 I-1), volume 2For abstract, see N76-16033.
Document ID
19760008946
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dziubala, T. (Rockwell Intern. Downey, Calif., United States)
Esparza, V. (Rockwell Intern. Downey, Calif., United States)
Gillins, R. L. (Rockwell Intern. Downey, Calif., United States)
Petrozzi, M. (Rockwell Intern. Downey, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
DMS-DR-2217-VOL-2
NASA-CR-141845
Report Number: DMS-DR-2217-VOL-2
Report Number: NASA-CR-141845
Accession Number
76N16034
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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