Aerothermal tests of a heat-pine-cooled leading edge at Mach 7
By: Charles J. Camarda, Langley Research Center
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper ; 1320
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 36
Subjects: Leading edges (Aerodynamics) -- Cooling
Notes: Nov. 1978

Includes bibliographical references