Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 120
Book Description
Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: General analysis and numerical examples, by P. V. Marrone
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 120
Book Description
Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966
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Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 144
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
An Analytical and Experimental Study of the Ionized Flow Field about a Hemisphere Cylinder and Its Effect on the Radiation Pattern of a Slot Antenna
Author: James T. CurtisPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 176
Book Description
A combined analytical and experimental investigation of the effect of stagnation region chemicalionization non-equilibrium phenomena on the aerothermodynamic and electrical properties of the flow field over a hemisphere cylinder at hypersonic speeds was conducted. In the analytical studies, flow field caluclations were made using several IBM 704 computer programs which account for finite reaction rate processes. The experimental phases of the study were done in the Cornell Aeronautical Laboratory 6' Shock Tunnel at a nominally constant velocity of 15,500 ft/sec. Measurements were made of the surface pressure and heat transfer, shock layer pitot pressure, and suface layer electrical conductivity on hemishpere cylinder models for a range of values of the stagnation region non-equilibrium scaling parameter. (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.
Study of High-density Hypervelocity Flows and Similitudes
Author: Cornell Aeronautical LaboratoryPublisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 320
Book Description
Proceedings of the Third Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight: Electrical properties of shock-ionized flow fields
Author: Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 366
Book Description
This volume is a collection of the unclassified papers presented at the Third Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight. This symposium consisted of the review of progress in reentry communication studies during the three year period since the prior meeting. The program of this symposium on plasma electromagnetics of hypersonic flight involves a wide range of scientific disciplines, including electromagnetics, aerodynamics, aero-thermochemistry, plasma dynamics, electronics, and high- temperature phenomena. The papers were selected to explore as many of these facets of research, including the results of laboratory, flight, and system tests, as time permitted.
Reaction Rates for High-temperature Air with Carbon and Sodium Impurities
Author: Mina L. CarnicomPublisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 156
Book Description
The values used by a number of investigators for the rate constants of high-temperature ([greater than or equal to]1000©K) homogeneous gaseous reactions involving species of the elements nitrogen, oxygen, carbon, and sodium have been compiled and are presented in tabular form. Included are reactions involving neutral species, charged species, free electrons, some species in excited electronic or vibrational states, and radiative processes.
SCR.
Author: Estimates of Nonequilibrium Ionization Phenomena in the Inviscid Apollo Plasma Sheath
Author: Michael G. DunnPublisher:
ISBN:
Category : Ionization
Languages : en
Pages : 76
Book Description