High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane--dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1
By: by Harold L. Robinson.
Series: NACA research memorandum ;; L8H05
Publisher: National Advisory Committee for Aeronautics
Published: 1948
Place of publication: Washington
Language: eng
Number of pages: 27
Subjects: Downwash (Aerodynamics); Airplanes -- Models -- Testing.; Wind tunnels.
Notes: Includes bibliographical references.
Cover title.