Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5
By: Theodore R. Creel, Jr., Barbara B. Holley, and Ivan E. Beckwith
Contributors: Holley, Barbara B; Beckwith, Ivan E; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 81935
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: 37
Subjects: Fluid mechanics
Notes: "Langley Research Center."

"May 1981"--Cover

Subject category 34

Includes bibliographical references