Use Of A Characteristic Surfaces For Unisymmetrical Supersonic Flow Problems
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Use Of A Characteristic Surfaces For Unsymmetrical Supersonic Flow Problems
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Author : Wolfgang E. Moeckel
language : en
Publisher:
Release Date : 1949
Use Of A Characteristic Surfaces For Unsymmetrical Supersonic Flow Problems written by Wolfgang E. Moeckel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.
Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.
The Method Of Characteristics For Three Dimensional Real Gas Flows
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Author : Charles R. Strom
language : en
Publisher:
Release Date : 1967
The Method Of Characteristics For Three Dimensional Real Gas Flows written by Charles R. Strom and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aerodynamics categories.
The method of characteristics is formulated for the computation of the supersonic flow of an inviscid, reacting gas over a smooth three-dimensional body. Various methods of constructing networks of bicharacteristic lines are examined from the point of view of numerical stability and accuracy. A new method of forming the network, which consists of projecting forward along streamlines from data points on specified data planes, is found to be most easily adopted to the particular requirements of nonequilibrium chemistry. The general method was coded for the IBM 7090 computer and the program demonstrated for the case of an ideal gas. Calculations were made for the case of an ideal gas. Calculations were made for the flow about a spherical-tip 15 degree half-angle cone at 10 degree angle of attack and a generalized elliptical body at zero incidence. Since the program yields the pressure distribution along specified streamlines, it is straightforward, in principle, to link it to a finite-rate chemistry stream tube program to treat three-dimensional, nonequilibrium flows. (Author).
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1952
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aeronautics categories.
Annual Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1955
Annual Report National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Report
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Author :
language : en
Publisher:
Release Date : 1955
Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1955
Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
A Study Of The Transient Behavior Of Shock Waves In Transonic Channel Flows
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Author : Robert V. Hess
language : en
Publisher:
Release Date : 1952
A Study Of The Transient Behavior Of Shock Waves In Transonic Channel Flows written by Robert V. Hess and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics categories.
The accuracy of the result obtained in a fundamental paper by Kantrowitz (NACA TN 1225) that a small short-time lowering of the back pressure in steady, shock-free, transonic diffuser flow causes a stationary or trapped shock to form near the critical sonic channel throat is investigated by considering the contribution of a higher-order term in the short-time calculations which was neglected in Kantrowitz's paper. In this higher approximation to the short-time effects, the shock is no longer stationary or trapped unless it is supported by a negative steady-flow back pressure; the result thus is no long in disagreement with steady-flow solutions for stationary shocks.
Theoretical And Analog Studies Of The Effects Of Nonlinear Stability Derivatives On The Longitudinal Motions Of An Aircraft In Response To Step Control Deflections And To The Influence Of Proportional Automatic Control
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Author : Benjamin Milwitzky
language : en
Publisher:
Release Date : 1955
Theoretical And Analog Studies Of The Effects Of Nonlinear Stability Derivatives On The Longitudinal Motions Of An Aircraft In Response To Step Control Deflections And To The Influence Of Proportional Automatic Control written by Benjamin Milwitzky and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Handbook Of Supersonic Aerodynamics
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Author : D. Adamson
language : en
Publisher:
Release Date : 1961
Handbook Of Supersonic Aerodynamics written by D. Adamson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic categories.
Handbook Of Supersonic Aerodynamics
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Author : Johns Hopkins University. Applied Physics Laboratory
language : en
Publisher:
Release Date : 1961
Handbook Of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic categories.