Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow

Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow
Author: Richard L. Humphrey
Publisher:
Total Pages: 60
Release: 1970
Genre: Cooling
ISBN:

Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 972
Release: 1964
Genre: Aeronautics
ISBN:

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Total Pages: 1152
Release: 1965
Genre: Aeronautics
ISBN:

NASA SP.

NASA SP.
Author:
Publisher:
Total Pages: 1150
Release: 1965
Genre: Aeronautics
ISBN: