Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps /
Louis G. Kaufman II.

Description

Main Author

Kaufman, Louis G.

Related Names

Air Force Flight Dynamics Laboratory (U.S.)
United States. Air Force.
Grumman Aircraft Engineering Corporation. Research Department

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963-1964.

Subjects

Wind tunnels
Wind tunnel models
Wedges
Schlieren photography
Reynolds number
Pressure
Heat > Heat / Transmission
Flow visualization
Aerodynamics, Hypersonic
Aerodynamic heating
Aerodynamic heating.
Wind tunnels.
Reynolds number.
Aerodynamics, Hypersonic.
Wind tunnel models.
Flow visualization.
Pressure.
Schlieren photography.
Heat > Heat / Transmission.
Wedges.

Summary

"Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for [M sub infinity =] 5 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for [M sub infinity =] 8 for Reynolds numbers between 1.1 and 3.3 million." -- page iii, pt.4.

Note

"Project No. 8219, Task No. 821902."
"September 1963", pt.1-2; "December 1963", pt.3; "July 1964", pt.4.

Physical Description

4 volumes : illustrations ; 28 cm.

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