Author: James Dewey Revell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180
Book Description
Second Order Theory for Unsteady Super-sonic Flow Past Slender, Pointed Bodies of Revolution
Author: James Dewey Revell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180
Book Description
The General Theory of Supersonic Flow Past Slender Pointed Bodies of Revolution
Author: M. J. Lighthill
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
First-order and Second-order Theory of Supersonic Flow Past Bodies of Revolution
Author: Milton D. Van Dyke
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Methods are studied for imporving the existing perturbation theories of axial and inclined supersonic flow past bodies of revolution. For axial flow, a second-order solution is developed using an interation procedure based upon the linearized solution. The resulting second-order problem is reduced to an equivalent first-order problem by discovery of a particular solution. The second-order supersonic flow can then be computed with slight modification of the Karman-Moore procedure. For inclined flow, no particular solution of the second-order equation has been discovered. The second-order solution is derived for a cone, and agrees well with the exact solution. The slender-body series expansion of the second-order solution is found to cause large inaccuracies in both the axial and inclined flows. The conclusion that first-order theory predicts the inclined flow no better than slender-body theory is shown to be erroneous. Non-linearity in lift is shown to result primarily from viscous separation of the crossflow along the after portions of the body. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Methods are studied for imporving the existing perturbation theories of axial and inclined supersonic flow past bodies of revolution. For axial flow, a second-order solution is developed using an interation procedure based upon the linearized solution. The resulting second-order problem is reduced to an equivalent first-order problem by discovery of a particular solution. The second-order supersonic flow can then be computed with slight modification of the Karman-Moore procedure. For inclined flow, no particular solution of the second-order equation has been discovered. The second-order solution is derived for a cone, and agrees well with the exact solution. The slender-body series expansion of the second-order solution is found to cause large inaccuracies in both the axial and inclined flows. The conclusion that first-order theory predicts the inclined flow no better than slender-body theory is shown to be erroneous. Non-linearity in lift is shown to result primarily from viscous separation of the crossflow along the after portions of the body. (Author).
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 482
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 482
Book Description
non- steady supersonic flow about pointed bodies of revolution
Author: w. h. dorrance
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Velocity Potential and Forces on Oscillating Slender Bodies of Revolution in Supersonic Flow Expanded to the Fifth Power of the Frequency
Author: Donald L. Lansing
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Research on Unsteady Transonic Flow Theory
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
Book Description
A Second-order Theory of Unsteady, Supersonic Flow
Author: Alan King King
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 376
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 376
Book Description
A Study of the Problem of Designing Airplanes with Satisfactory Inherent Damping of the Dutch Roll Oscillation
Author: Anatol Roshko
Publisher:
ISBN:
Category : Aerial spraying and dusting in agriculture
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Aerial spraying and dusting in agriculture
Languages : en
Pages : 258
Book Description
Manual on Aeroelasticity
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 716
Book Description
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 716
Book Description