Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage
By: Ronald J. Steinke.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4141.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 14
Subjects: Viscous flow -- Computer simulation.; Unsteady flow (Aerodynamics) -- Computer simulation.; Turbomachines -- Aerodynamics -- Computer simulation.; Turbomachines -- Design and construction.; Aerodynamics, Supersonic.; Computer programs.; Rotor blades.; Supersonic flow.; Turbomachinery.; Unsteady flow.; Viscous flow.
Other titles: Application of a two dimensional unsteady viscous analysis code to a supersonic throughflow fan stage.
Notes: Shipping list no.: 90-0561-M.

"Performing organization report no.: E-4848"--Technical rept. documentation p.

Includes bibliographical references (p. 14).

Also available via Internet from the NASA Technical Report Server web site. Address as of 5/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004071%5F1990004071.pdf; current access available via PURL.

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

505-62-21.