Support Wire Disturbances in Near Viscous Wakes of Slender Supersonic Bodies

Author

K. A. Mirly
B. P. Selberg, Missouri University of Science and TechnologyFollow

Abstract

The viscous wake properties of slender bodies suspended by wire were experimentally investigated. Schlieren observations plus the measurements of pitot pressures behind a flat plate and an axisymmetric cone at Mach 3. 15 were used for this purpose. Conclusions resulting from these investigations are presented.

Recommended Citation

K. A. Mirly and B. P. Selberg, "Support Wire Disturbances in Near Viscous Wakes of Slender Supersonic Bodies," Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics (AIAA), Jan 1973.

The definitive version is available at https://doi.org/10.2514/3.27768

Department(s)

Mechanical and Aerospace Engineering

International Standard Serial Number (ISSN)

0022-4650

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1973 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.

Publication Date

01 Jan 1973