Interactive calculation procedures for mixed compression inlets
By: Eli Reshotko.
Contributors: United States. National Aeronautics and Space Administration.; Case Western Reserve University. Dept. of Mechanical & Aerospace Engineering.
Series: NASA contractor report -- NASA CR-186581.
Publisher: Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University
Published: 1983
Place of publication: Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Laminar boundary layer.; Nacelles.; Oblique shock waves.; Shock wave interaction.; Supersonic aircraft.; Turbulent boundary layer.
Notes: Shipping list no.: 1991-0039-M.

"Final technical report."

"March 1983."

"NASA grant NAG 3-140."

Includes bibliographical references.

Also available via Internet from the NTRS web site. Address as of 6/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016618%5F1990016618.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1990. 1 microfiche.