Author: M. Leroy SpearmanPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Some Effects of Wing and Body Geometry on the Aerodynamic Characteristics of Configurations Designed for High Supersonic Mach Numbers
Author: M. Leroy SpearmanPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63
Author: Maurice O. FerynPublisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
Author: A. Warner RobinsPublisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68
Book Description
The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4
Author: Stuart L. TreonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2
Author: Ross B. RobinsonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87
Author: Royce L. McKinneyPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70
Author: Walter P. NelmsPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82
Book Description
Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6
Author: Walter P. NelmsPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 108
Book Description
Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The configuration had a delta planform with an elliptic cone forebody and an afterbody of elliptic cross section. Detailed effects of varying angle of attack (-2 to 15 deg), angle of sideslip (-2 to 8 deg), Mach number, and configuration buildup were considered. In addition, the effectiveness of horizontal tail, vertical tail, and canard stabilizing and control surfaces was investigated. The results indicate that all configurations were longitudinally stable near maximum lift drag ratio. The configurations with vertical tails were directionally stable at all angles of attack. Trim penalties were small at hypersonic speeds for a center of gravity location representative of the airplane, but because of the large rearward travel of the aerodynamic center, trim penalties were severe at transonic Mach numbers.
NASA Scientific and Technical Publications
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410
Book Description
Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63
Author: James F. CampbellPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
