In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0
By: David F. Fisher, N. Sam Dougherty, Jr
Contributors: Dougherty, N. Sam; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Dryden Flight Research Facility; Arnold Research Organization
Series: NASA technical paper -- 1971
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 140
Subjects: Boundary layer; Mach number
Notes: "June 1982"--Cover

"Ames Research Center, Dryden Flight Research Facility."

"Arnold Research Organization, Inc."

Includes bibliographical references