Effects of Acceleration and Pitch Variations on a Rotating Wing
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 671-681
2012-01-01
11 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aerodynamics of rotating-wing aircraft with blade-pitch control
TIBKAT | 1940
|Pitch Rate Effects on Delta Wing Vortex Breakdown
AIAA | 1997
|Pitch Rate Effects on Delta Wing Vortex Breakdown
Online Contents | 1996
|Pitch Rate Effects on Delta Wing Vortex Breakdown
Online Contents | 1997
|