Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 62
Book Description
Hypersonic Aerodynamic Characteristics of Plain and Ported Elevon Controls on a 75 Deg Swept Modified Delta-wing Configuration
Author: Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations
Author: Theodore J. GoldbergPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 108
Book Description
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by
Author: John W. PaulsonPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2
Author: Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 Deg Swept Delta Wing
Author: J. A. PenlandOn the Hypersonic Flow Over a Delta Wing with Very Supersonic Leading Edges
Author: Norman D. MalmuthPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 66
Book Description
For the case of very supersonic leading edges, the inviscid hypersonic flow over the windward side of a symmetrical flat-plate delta wing at incidence is analyzed. The limit selected is that the incidence is of higher order than the aspect ratio as the incidence tends to zero at infinite Mach number. In this framework, the flow regions consist of a two-dimensional domain adjacent to the leading edges and a central conefield. The flow quantities in the central region represent small linear, rotational perturbations about the zero sweep flow. A Riemann-Poincare boundary value problem for the pressure perturbation is formulated. An additional condition involving the sidewash at the shock is found to be required to resolve the indeterminacy of the foregoing boundary value problem. Series solutions and numerical results are presented for the shock shape and the pressure. The behavior of the latter quantity is found to be similar to that given by the irrotational linear solution for the supersonic leading edge case. Finally, the relationship between the present application and others involving diffraction problems and corner flows is indicated.
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 SpencerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
Book Description
Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 ̊swept Delta Wing
Author: Jim A. PenlandPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 84
Book Description
An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow
Author: Mitchel H. BertramPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 134
Book Description
An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels
Author: Bernard SpencerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.