Boundary-layer transition on the N.A.C.A. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel

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Boundary-layer transition on the N.A.C.A. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel

Boundary-layer transition on the N.A.C.A. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel

Becker, John V.

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Title :

Boundary-layer transition on the N.A.C.A. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel

Contributors:

Becker, John V. (author)

Published in:

Wartime report ; L-682

Publication date :

1940

Size :

26 S., [11] Bl.

Remarks:

Ill., graph. Darst.
Originally issued January 1940 as Advance confidential report

Type of media :

Report

Type of material :

Print

Language :

English

Keywords :

Strömungsmesstechnik , NACA-Profil

Classification :

BKL:

50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik

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