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
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).
non- steady supersonic flow about pointed bodies of revolution
NASA Technical Note
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
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
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