Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) /

Bibliographic Details

Main Author:	Marroquin, J. (Author)
Corporate Author:	Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services
Format:	Government Document eBook
Language:	English
Published:	Houston, Texas : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, March 1985.
Series:	NASA contractor report ; NASA CR-167695.
Subjects:	Aerothermodynamics. Hypersonic heat transfer. Aerodynamic heat transfer. Hypersonic speed. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo107998