Author: Warren Jr GillespiePublisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces
Author: Warren Jr GillespieLift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces
Author: Warren Jr GillespieLongitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing
Author: Rowe Jr ChapmanLongitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing
Author: Edward J. RayDrag Due to Lift at Mach Numbers Up to 2.0
Author: Edward C. PolhamusPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between Plus Or Minus 6.5 Degrees
Author: Warren Jr GillespieAerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing
Author: Lift and Drag Characteristics at Subsonic Speeds and at a Mach Number of 1.9 of a Lifting Circular Cylinder with a Fineness Ratio of 10
Author: Vernard E. LockwoodPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26
Book Description
A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33
Author: Robert F. PeckLaunch, Low-speed, and Landing Characteristics Determined from the First Flight of the North American X-15 Research Airplane
Author: Thomas W. FinchPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30
Book Description