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Accession Number:
AD0838727
Title:
TEST REPORT FOR PHASE III OF THE AERODYNAMIC HEATING TEST AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL,
Corporate Author:
GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
Report Date:
1959-07-02
Abstract:
The primary purpose of the test was to determine the effect of variously shaped protuberances on the convective heat transfer coefficients for a flat plate in turbulent supersonic flow. The secondary objective of the test was to determine the convective heat transfer coefficients for the surfaces of the protuberance models. The model configurations tested were the plain flat plate, 2 in. x 4 in. flange, 30 deg. wedge 14 cylinder, 1 in. x 2 in. flange, 2.8 in. D swept cylinders, and 2.8 in. D vertical cylinders. Author
Pages:
0445
Distribution Statement:
Availability: microfiche copies only.
Contract Number:
AF 04(645)-4
File Size:
0.00MB
