Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft
By: Frank M. Anthony and Robert G. Helenbrook ; prepared for Langley Research Center under contract NAS1-12806
Contributors: Helenbrook, Robert G; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA contractor report -- 3403
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 79
Subjects: Thermal stresses
Notes: "February 1981."

Subject category 39

Includes bibliographical references