Experimental and theoretical investigations in two-dimensional transonic flow.Experimental and theoretical results are presented from a study of the flow over a family of transonically scaled circular-arc bodies mounted in a solid-wall wind tunnel. Data are presented for Reynolds numbers between 30,000 and 3,600,000, based on chord. The high Reynolds number results are compared with computations based on inviscid theory, and are used to investigate transonic similarity and the behavior of the flow near choking. The results at low Reynolds number are used to demonstrate the effect of viscosity on the overall flowfield, and comparisons are made with existing laminar viscous/inviscid interaction theory.
Document ID
19730051411
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Collins, D. J. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Krupp, J. A. (California, University Los Angeles, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 73-659Report Number: AIAA PAPER 73-659
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Palm Springs, CA
Start Date: July 16, 1973
End Date: July 18, 1973
Sponsors: American Institute of Aeronautics and Astronautics