Determination of the pressure drag of airfoils by integration of surface pressures
By: Williams H. Phillips.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 102722.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1990
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airfoil profiles.; Boundary layer flow.; Flow distribution.; Pressure drag.; Subsonic flow.
Notes: Distributed to depository libraries in microfiche.

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