Second Order Theory for Unsteady Super-sonic Flow Past Slender, Pointed Bodies of Revolution

Second Order Theory for Unsteady Super-sonic Flow Past Slender, Pointed Bodies of Revolution PDF Author: James Dewey Revell
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180

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Second Order Theory for Unsteady Super-sonic Flow Past Slender, Pointed Bodies of Revolution

Second Order Theory for Unsteady Super-sonic Flow Past Slender, Pointed Bodies of Revolution PDF Author: James Dewey Revell
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 180

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The General Theory of Supersonic Flow Past Slender Pointed Bodies of Revolution

The General Theory of Supersonic Flow Past Slender Pointed Bodies of Revolution PDF Author: M. J. Lighthill
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ISBN:
Category :
Languages : en
Pages :

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First-order and Second-order Theory of Supersonic Flow Past Bodies of Revolution

First-order and Second-order Theory of Supersonic Flow Past Bodies of Revolution PDF Author: Milton D. Van Dyke
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ISBN:
Category :
Languages : en
Pages : 29

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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

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 482

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non- steady supersonic flow about pointed bodies of revolution

non- steady supersonic flow about pointed bodies of revolution PDF Author: w. h. dorrance
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ISBN:
Category :
Languages : en
Pages : 38

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Velocity Potential and Forces on Oscillating Slender Bodies of Revolution in Supersonic Flow Expanded to the Fifth Power of the Frequency

Velocity Potential and Forces on Oscillating Slender Bodies of Revolution in Supersonic Flow Expanded to the Fifth Power of the Frequency PDF Author: Donald L. Lansing
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

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Research on Unsteady Transonic Flow Theory

Research on Unsteady Transonic Flow Theory PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116

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A Second-order Theory of Unsteady, Supersonic Flow

A Second-order Theory of Unsteady, Supersonic Flow PDF Author: Alan King King
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ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 376

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A Study of the Problem of Designing Airplanes with Satisfactory Inherent Damping of the Dutch Roll Oscillation

A Study of the Problem of Designing Airplanes with Satisfactory Inherent Damping of the Dutch Roll Oscillation PDF Author: Anatol Roshko
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ISBN:
Category : Aerial spraying and dusting in agriculture
Languages : en
Pages : 258

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Manual on Aeroelasticity

Manual on Aeroelasticity PDF Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 716

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