A method of computing the resistance of a cascade of airfoils in a viscous compressible gas flow is described. The investigation occurred in subsonic velocities only because of the required assumption of isentropic flow.
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Parallel Title:
Soprotivlenie reshetki profilei v gazovom potoke s dokriticheskimi skorostiami
Description
A method of computing the resistance of a cascade of airfoils in a viscous compressible gas flow is described. The investigation occurred in subsonic velocities only because of the required assumption of isentropic flow.
This report is part of the following collections of related materials.
National Advisory Committee for Aeronautics Collection
The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).
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Loitsianskii, L. G.Resistance of cascade of airfoils in gas stream at subsonic velocity,
report,
September 1951;
(https://digital.library.unt.edu/ark:/67531/metadc62996/:
accessed April 24, 2024),
University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu;
crediting UNT Libraries Government Documents Department.