Author: James L. DillonPublisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68
Book Description
Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane
Author: James L. DillonPublisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68
Book Description
Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 ̊swept Delta Wing
Author: Louis E. ClarkPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 68
Book Description
Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane
Author: James L. DillonPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52
Book Description
Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70° Swept Delta Wing
Author: Louis E. ClarkAerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane
Author: James L. DillonAerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Delta Wing
Author: L. E. ClarkAerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of Wing-body Design Concept for a Hypersonic Research Airplane
Author: James L. DillonPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82
Book Description
Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 Degrees Swept Delta Wing
Author: Louis E. ClarkPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 58
Book Description
Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86
Author: William John SmallPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781725609662
Category :
Languages : en
Pages : 32
Book Description
Longitudinal aerodynamic characteristics for a hydrogen-fueled hypersonic transport concept at Mach 6 are presented. The model components consist of four bodies with identical longitudinal area distributions but different cross-sectional shapes and widths, a wing, horizontal and vertical tails, and a set of wing-mounted nacelles simulated by slid bodies on the wing upper surface. Lift-drag ratios were found to be only sightly affected by fuselage planform width or cross sectional shape. Relative distribution of fuselage volume above and below the wing was found to have an effect on the lift-drag ratio, with a higher lift drag ratio produced by the higher wing position. Riebe, G. D. Langley Research Center NASA-TP-2235, L-15675, NAS 1.60:2235 RTOP 505-43-23-10...