Comparison of experimental and theoretical design parameters of a 6-inch-diameter annular jet model with a jet angle of -45deg. hovering in proximity to the ground; and experimental results for forward flight at zero angle of attack.
Contributors: David W. Taylor Model Basin. Aerodynamics Laboratory.
Series: Aerodynamics Laboratory research and development report; Report 1376; Aero report 954; TED No. TMB AD-3242
Publisher: David Taylor Model Basin
Published: 1959
Place of publication: [s.l.]
Language: eng