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Accession Number:
ADB805606
Title:
The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight
Descriptive Note:
Technical rept.
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER
Report Date:
1947-07-01
Pagination or Media Count:
13.0
Abstract:
Distribution Statement:
APPROVED FOR PUBLIC RELEASE