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Inviscid Nonequilibrium Flow Behind Bow And Normal Shock Waves
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Book Synopsis Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 by : Cornell Aeronautical Laboratory
Download or read book Inviscid, Nonequilibrium Flow Behind Bow and Normal Shock Waves: The revised normal shock program, by Leonard J. Garr [and others] 1966 written by Cornell Aeronautical Laboratory and published by . This book was released on 1966 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Estimate of the Chemical Kinetics Behind Normal Shock Waves in Mixtures of Carbon Dioxide and Nitrogen for Conditions of Mars Entry by : Robert L. McKenzie
Download or read book An Estimate of the Chemical Kinetics Behind Normal Shock Waves in Mixtures of Carbon Dioxide and Nitrogen for Conditions of Mars Entry written by Robert L. McKenzie and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres by : William L. Gose
Download or read book A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres written by William L. Gose and published by . This book was released on 1971 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate inverse solution is presented for the nonequilibrium flow in the inviscid shock layer about a vehicle in hypersonic flight. The method is based upon a thin-shock-layer approximation and has the advantage of being applicable to both subsonic and supersonic regions of the shock layer. The relative simplicity of the method makes it ideally suited for programming on a digital computer with a significant reduction in storage capacity and computing time required by other more exact methods. Comparison of nonequilibrium solutions for an air mixture obtained by the present method is made with solutions obtained by two other methods. Additional cases are presented for entry of spherical nose cones into representative Venusian and Martian atmospheres. A digital computer program written in FORTRAN language is presented that permits an arbitrary gas mixture to be employed in the solution. The effects of vibration, dissociation, recombination, electronic excitation, and ionization are included in the program.
Book Synopsis Computations of the Nonequilibrium Flow of a Viscous, Radiating Fluid about a Blunt Axisymmetric Body by : J. T. Curtis
Download or read book Computations of the Nonequilibrium Flow of a Viscous, Radiating Fluid about a Blunt Axisymmetric Body written by J. T. Curtis and published by . This book was released on 1967 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock-wave Shapes and Surface Pressures on Hemisphere- and Cone-cylinders in Low-density Hypersonic Flow Including Ablation by : Daryl J. Monson
Download or read book Shock-wave Shapes and Surface Pressures on Hemisphere- and Cone-cylinders in Low-density Hypersonic Flow Including Ablation written by Daryl J. Monson and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Also available online.
Download or read book NASA Technical Note written by and published by . This book was released on 1974 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 992 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Simplified Molecular Model for Studying Vibration-dissociation Coupling in Fluid Flows by : Walter Albert Reinhardt
Download or read book A Simplified Molecular Model for Studying Vibration-dissociation Coupling in Fluid Flows written by Walter Albert Reinhardt and published by . This book was released on 1969 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simplified mathematical model is derived that is useful for studying the effects of vibration-dissociation coupling in fluid flows. The derivation is based on energy-moment procedure for simplifying the master equations. To obtain the model equations it is assumed that the vibrational energy can be approximated by the introduction of two vibrational temperatures. The effects of molecular anharmonicity are also accounted for in an approximate manner. The parameters contained within the equations are evaluated by making comparisons with experimental data. It is shown that the model contains the minimum required structure allowing favorable agreement with existing experimental data. Numerical solutions are given for the quasi-steady zone behind a normal shock wave, for the complete structure of a shock wave, and for nozzle flow. The results provide the appropriate pre-exponential temperature dependence of the effective dissociation rate, yield and induction time before dissociation is observed, and, in the case of expanding flow, yield one-fourth less effective relaxation time than the Landau-Teller theory. The thermodynamic quantities for the vibrational mode (partition function, internal energy, and specific heat) agree accurately with like quantities evaluated from spectroscopic data. By the introduction of appropriate assumptions it is shown that the equations reduce to a form identical to the Marrone-Treanor model except for a "truncation factor". When the vibrational temperatures are not large, the model is identical to that of Landau and Teller. The numerical procedure used to integrate the system of rate and flow equations is also described.
Book Synopsis General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics by : David A. Bittker
Download or read book General Chemical Kinetics Computer Program for Static and Flow Reactions, with Application to Combustion and Shock-tube Kinetics written by David A. Bittker and published by . This book was released on 1972 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt: A general chemical kinetics program is described for complex, homogeneous ideal-gas reactions in any chemical system. Its main features are flexibility and convenience in treating many different reaction conditions. The program solves numerically the differential equations describing complex reaction in either a static system or one-dimensional inviscid flow. Applications include ignition and combustion, shock wave reactions, and general reactions in a flowing or static system. An implicit numerical solution method is used which works efficiently for the extreme conditions of a very slow or a very fast reaction. The theory is described, and the computer program and users' manual are included.
Book Synopsis NASA Technical Report by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1969 with total page 880 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Attached and Separated Boundary Layers on Highly Cooled, Ablating and Nonablating Models at M by : Donald M. Kuehn
Download or read book Attached and Separated Boundary Layers on Highly Cooled, Ablating and Nonablating Models at M written by Donald M. Kuehn and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Two Different Interpretations of Measured Dissociation-rate Constants and Their Effects on Coupled Vibrational-dissociational Flows of Oxygen Over a Wedge by : Fred R. DeJarnette
Download or read book Two Different Interpretations of Measured Dissociation-rate Constants and Their Effects on Coupled Vibrational-dissociational Flows of Oxygen Over a Wedge written by Fred R. DeJarnette and published by . This book was released on 1967 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Blunt Body Solutions for Spheres and Ellipsoids in Equilibrium Gas Mixtures by : Mamoru Inouye
Download or read book Blunt Body Solutions for Spheres and Ellipsoids in Equilibrium Gas Mixtures written by Mamoru Inouye and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Inverse-method Solution for Radiating, Nonadiabatic, Equilibrium Inviscid Flow Over a Blunt Body by : Ralph A. Falanga
Download or read book An Inverse-method Solution for Radiating, Nonadiabatic, Equilibrium Inviscid Flow Over a Blunt Body written by Ralph A. Falanga and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : James T. Curtis
Download or read book 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 written by James T. Curtis and published by . This book was released on 1963 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Book Synopsis Estimates of Nonequilibrium Ionization Phenomena in the Inviscid Apollo Plasma Sheath by : Michael G. Dunn
Download or read book Estimates of Nonequilibrium Ionization Phenomena in the Inviscid Apollo Plasma Sheath written by Michael G. Dunn and published by . This book was released on 1966 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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