Author: S. Levy
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 642
Book Description
Determination of Influence Coefficients
Determination of Influence Coefficients by S.Levy
Structural Analysis- Influence Coefficient Method
Author: Radha Kanta Sarkar
Publisher:
ISBN:
Category : Structural analysis (Engineering)
Languages : en
Pages : 430
Book Description
Publisher:
ISBN:
Category : Structural analysis (Engineering)
Languages : en
Pages : 430
Book Description
A Method of Determining Aerodynamic-influence Coefficients from Wind-tunnel Data for Wings at Supersonic Speeds
Author: Patrick A. Gainer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40
Book Description
A Comparison of Two Interaction Methods for the Determination of Influence Coefficients for Aircraft Swept Beams
Structural Analysis- Influence Coefficient Method
Author: Radha Kanta Sarkar
Publisher:
ISBN:
Category : Structural analysis (Engineering)
Languages : en
Pages : 430
Book Description
Publisher:
ISBN:
Category : Structural analysis (Engineering)
Languages : en
Pages : 430
Book Description
Report - Naval Ship Research and Development Center
Author: David W. Taylor Naval Ship Research and Development Center
Publisher:
ISBN:
Category : Shipbuilding
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Shipbuilding
Languages : en
Pages : 28
Book Description
Simplified Method for Determination of Critical Height of Distributed Roughness for Boundary-layer Transition at Mach Numbers from 0 to 5
Author: Albert L. Braslow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
Linear Structural Analysis
Author: Peter Beaumont Morice
Publisher:
ISBN:
Category : Framing (Building)
Languages : en
Pages : 192
Book Description
Publisher:
ISBN:
Category : Framing (Building)
Languages : en
Pages : 192
Book Description
Influence Coefficients for Circular Plates
Author: Kerry S. Havner
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 122
Book Description
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 122
Book Description