Effects of Some Wing Variations Including Wingtip Deflection on the Static Longitudinal Aerodynamic Characteristics of a Delta-wing Configuration at Supersonic Speeds Author: Publisher: Published: 1960 Total Pages: 52 ISBN-13: DOWNLOAD EBOOK →
Effects of Some Wing Variation Including Wing Tip Deflection on the Static Longitudinal Aerodynamic Characteristics of a Delta Wing Configuration at Supersonic Speeds Author: Robert W. Dunning Publisher: Published: 1960 Total Pages: 47 ISBN-13: DOWNLOAD EBOOK →
The Effects of Wing-tip Droop on the Aerodynamic Characteristics of a Delta-wing Aircraft at Supersonic Speeds Author: Publisher: Published: 1960 Total Pages: 48 ISBN-13: DOWNLOAD EBOOK →
The Effects of Wing-tip Droop on the Aerodynamic Characteristics of a Delta-wing Aircraft at Supersonic Speeds Author: Richard H. Peterson Publisher: Published: 1960 Total Pages: 52 ISBN-13: DOWNLOAD EBOOK →
Longitudinal Aerodynamic Characteristics at Low Subsonic Speeds of a Highly Swept Delta Wing Utilizing Nose Deflection for Control Author: Bernard Spencer Publisher: Published: 1962 Total Pages: 32 ISBN-13: DOWNLOAD EBOOK →
High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° Author: Bernard Spencer Publisher: Published: 1959 Total Pages: 34 ISBN-13: DOWNLOAD EBOOK →
High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0 Deg to 90 Deg Author: Publisher: Published: 1959 Total Pages: 32 ISBN-13: DOWNLOAD EBOOK →
Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels Author: M. Leroy Spearman Publisher: Published: 1961 Total Pages: 36 ISBN-13: DOWNLOAD EBOOK →
Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Thick Delta Wing Hypersonic Glider Configuration for Angles of Attack Up to 100 Deg Author: Publisher: Published: 1961 Total Pages: 40 ISBN-13: DOWNLOAD EBOOK →
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 Author: Robert S. Osborne Publisher: Published: 1960 Total Pages: 20 ISBN-13: DOWNLOAD EBOOK →