The Online Books Page

Downwash

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

• Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40 (National Aeronautics and Space Administration, 1959), by Louis S. Stivers and Ames Research Center (page images at HathiTrust)
• Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps (National Aeronautics and Space Administration, 1959), by James A. Weiberg, V. Robert Page, and Ames Research Center (page images at HathiTrust)
• Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46 (National Aeronautics and Space Administration, 1959), by Frank J. Centolanzi and Ames Research Center (page images at HathiTrust)

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