Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
The Effect of Camber on the Aerodynamic Characteristics of a Body at a Mach Number of 2.01
Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 484
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 484
Book Description
Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82
Author: Ross B. Robinson
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 42
Book Description
A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance
Author: Donald L. Loving
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 92
Book Description
Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control
Author: Roger H. Fournier
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 76
Book Description
An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 76
Book Description
An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Effect of a Variable Camber and Twist Wing at Transonic Mach Numbers
Author: James C. Ferris
Publisher:
ISBN:
Category : Transonic planes
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Transonic planes
Languages : en
Pages : 60
Book Description
Effect Opf Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20
Author: Clyde Hayes
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Book Description