Author: J. T. CurtisPublisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 166
Book Description
Computations of the Nonequilibrium Flow of a Viscous, Radiating Fluid about a Blunt Axisymmetric Body
Author: J. T. CurtisPublisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 166
Book Description
Computation of Equilibrium Hypersonic Flow about Blunt Axisymmetric Bodies with Sharp Concers
Author: J. T. CurtisPublisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 144
Book Description
Scientific and Technical Aerospace Reports
Author: Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Science
Languages : en
Pages : 784
Book Description
Government-wide Index to Federal Research & Development Reports
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Book Description
The Method of Characteristics for Three-dimensional Real-gas Flows
Author: Charles R. StromPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 136
Book Description
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).
Analytical Comparison of Hypersonic Flight and Wind Tunnel Viscous/inviscid Flow Fields
Author: H. J. FivelPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 130
Book Description
Government-wide Index to Federal Research & Development Reports
Author: Inverse-method and Method-of-characteristics Flow-field Programs
Author: J. B. MorenoPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 136
Book Description
Two flow-field computer codes are described. The codes were developed to compute the flow about blunt axisymmetric or two-dimensional bodies moving with supersonic speeds at zero angle of attack. Boundary-layer effects and a variety of thermochemical options are included. A pair of auxiliary codes for machine-plotting the flow-field results is also described.
Author: