Anderson, O. L. (1974). Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts. National Aeronautics and Space Administration.
Chicago Style (17th ed.) CitationAnderson, O. L. Finite-difference Solution for Turbulent Swirling Compressible Flow in Axisymmetric Ducts with Struts. Washington, D.C.: National Aeronautics and Space Administration, 1974.
MLA (9th ed.) CitationAnderson, O. L. Finite-difference Solution for Turbulent Swirling Compressible Flow in Axisymmetric Ducts with Struts. National Aeronautics and Space Administration, 1974.
Warning: These citations may not always be 100% accurate.