A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels /
by C.J. Schueler.

Description

Main Author

Schueler, C. J.

Related Names

ARO, Inc.
Arnold Engineering Development Center
United States. Air Force.

Language(s)

English

Published

Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963.

Subjects

Noses (Aircraft)
Boundary layer.
Aerodynamics, Supersonic.

Note

Report prepared by ARO, Inc., a subsidiary of Sverdrup and Parcel, Inc.
"March 1963."

Physical Description

22 pages : illustrations, 28 cm

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