Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of Thin-trapezoidal-wing-body Combination at Mach Number of 1.43 [with List of References]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of a Thin-trapezoidal-wing-body Combination at a Mach Number of 1.43
Author: Thomas C. Kelly
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
The Effects of Wing Incidence on the Aerodynamic Loading Characteristics of a Sweptback Wing-body Combination at Transonic Speeds
Author: Harold L. Robinson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94
Book Description
A Method for Calculating Aerodynamic Loadings on Thin Wings at a Mach Number of 1
Author: John L. Crigler
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing
Author: Harry W. Carlson
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Loading of Swept and Unswept Wings
Author: Franklin W. Diederich
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 110
Book Description
Charts are presented for the estimation of aeroelastic effects on spanwise lift distribution, lift-curve slope, aerodynamic career, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this paper are discussed.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 110
Book Description
Charts are presented for the estimation of aeroelastic effects on spanwise lift distribution, lift-curve slope, aerodynamic career, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this paper are discussed.
Effects of Wing Section and Body Vertical Location on the Longitudinal Aerodynamic Characteristics at Mach Number 4.63 of a Configuration Having a 70 Deg Delta Wing and a Low Volume Body
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow
Author: Charlie M. Jackson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.
Calculation of Aerodynamic Loading and Twist Characteristics of Flexible Wing at Mach Numbers Approaching 1.0 and Comparison with Experiment [with List of References]
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 17
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 17
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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description