The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
By: E.B. Plentovich.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2537.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; National Technical Information Service, distributor]
Published: 1986
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airfoils.; Boundary layer stability.; Errors.; Orifices.; Static pressure.; Transonic flow.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1 microfiche.