High Reynolds number, low Mach number, steady flow field calculations over a NACA 0012 airfoil using Navier-Stokes and Interactive Boundary Layer theory
Contributors: Platzer, Max Franz
Published: 1987
Language: eng
Number of pages: 106
Subjects: Aeronautics
Notes: Thesis advisor, Max Franz Platzer.

Available from National Technical Information Service, Springfield, Va.

ADA189871.

Thesis (M.S. in A.E.) Naval Postgraduate School, Dec. 1987.

Includes bibliographical references.

c.1, c.2