Wind tunnel tests of supersonic two-dimensional and half-axisymmetric inlet models in a nonuniform flow field at Mach numbers from 1.5 through 2.5 /
Frederick K. Hube and Leroy M. Jenke.

Description

Main Author

Hube, Frederick K.

Related Names

Jenke, Leroy M., author.
ARO, Inc.
Arnold Engineering Development Center
United States. Air Force.

Language(s)

English

Published

Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971.

Subjects

Aerodynamics, Supersonic.
Two-phase flow.
Jet engines > Jet engines / Air intakes > Jet engines / Air intakes / Testing.

Note

Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
Final Report: October 15 through November 18, 1970."
"May 1971."

Physical Description

136 pages : illustrations ; 28 cm

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