The peak pressure rise across an oblique shock emerging from a turbulent boundary layer over a plane surface
By: Luigi Crocco and Ronald F. Probstein.
Contributors: Probstein, Ronald F.; Princeton University. Dept. of Aeronautical Engineering; U.S. Air Force. Office of Scientific Research; U.S. Office of Naval Research
Series: Princeton University. Dept. of Aeronautical Engineering. Report -- 254
Publisher: Princeton University, Dept. of Aeronautical Engineering
Published: 1954
Place of publication: [Princeton, N.J.]
Number of pages: 28
Notes: Order no. 6.

Project no. NR-061-049.

Bibliographical references: p. 24-25.

Contract number: N60onr-270