The Online Books Page

Incompressible flow

See also what's at your library, or elsewhere.

• A viscous/potential flow interaction analysis method for multi-element infinite swept wings. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust)
• A method for analyzing dynamic stall of helicopter rotor blades / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Peter Crimi, Barry L. Reeves, Langley Research Center, and Avco Corporation (page images at HathiTrust)
• A numerical study of confined turbulent jets / (Washington, D.C. : National Aeronautics and Space Administration ; [Hanover, Md.] : NASA Center for Aerospace Information [distributor], 1993), by J. Zhu, T. H. Shih, Lewis Research Center, American Society of Mechanical Engineers, and Louisiana) Winter Annual Meeting (1993 : New Orleans (page images at HathiTrust)
• A note on the wave action density of a viscous instability mode on a laminar free-shear flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994), by Thomas F. Balsa and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by E. Widmayer, S. A. Clevenston, W. T. Lauten, and Langley Research Center (page images at HathiTrust)
• Compressible flow through a porous plate /, by George Emanuel, John P. Jones, sponsor Aerospace Corporation. Laboratory Operations, and issuing body United States. Air Force. Systems Command. Space Systems Division (page images at HathiTrust)

Items below (if any) are from related and broader terms.