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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 3
- Publication Year :
- 1975
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1975.
-
Abstract
- For abstract, see N76-16033.
- Subjects :
- Aerodynamics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NAS9-13247
- Publication Type :
- Report
- Accession number :
- edsnas.19760008947
- Document Type :
- Report