Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
By: Venkit Iyer.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA contractor report -- 4269.; NASA contractor report -- NASA CR-4269.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; National Technical Information Service, distributor]
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer equations.; Comppressible boundary layer.; Computational fluid dynamics.; Flow distribution.; Fuselages.; Three dimensional boundary layer.; Wing profiles.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0855-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 3 microfiches.