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

Personal Author(s):

Report Date:

1947-07-01

Pagination or Media Count:

13.0

Abstract:

Subject Categories:

  • Aerodynamics
  • Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE