Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel
By: Ivan E. Beckwith ... [et al.]
Contributors: Beckwith, Ivan E; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2180
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 67
Subjects: Boundary layer; Supersonic wind tunnels
Notes: Distributed to depository libraries in microfiche

"September 1983"--Cover

Subject category 34

Includes bibliographical references