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A Simplified Molecular Model for Studying Vibration-dissociation Coupling in Fluid Flows
  • Language: en
  • Pages: 340

A Simplified Molecular Model for Studying Vibration-dissociation Coupling in Fluid Flows

  • Type: Book
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  • Published: 1969
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  • Publisher: Unknown

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...

NASA Technical Report
  • Language: en
  • Pages: 880

NASA Technical Report

  • Type: Book
  • -
  • Published: 1969
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  • Publisher: Unknown

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NASA Technical Note
  • Language: en
  • Pages: 470

NASA Technical Note

  • Type: Book
  • -
  • Published: 1971
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  • Publisher: Unknown

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Index of Patents Issued from the United States Patent Office
  • Language: en
  • Pages: 2220

Index of Patents Issued from the United States Patent Office

  • Type: Book
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  • Published: 1972
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  • Publisher: Unknown

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Proceedings of the Grand Chapter of Royal Arch Masons of the State of California at Its ... Annual Convocation
  • Language: en
  • Pages: 622
A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres
  • Language: en
  • Pages: 164

A Thin-shock-layer Solution for Nonequilibrium, Inviscid Hypersonic Flows in Earth, Martian, and Venusian Atmospheres

  • Type: Book
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  • Published: 1971
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  • Publisher: Unknown

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.

Vibrational Relaxation and Radiative Gain in Expanding Flows of Anharmonic Oscillators
  • Language: en
  • Pages: 36

Vibrational Relaxation and Radiative Gain in Expanding Flows of Anharmonic Oscillators

  • Type: Book
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  • Published: 1971
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  • Publisher: Unknown

The set of master rate equations for the vibrational relaxation of mixtures of anharmonic diatomic gases in supersonic nozzle expansions is integrated numerically. Large deviations from a Boltzmann distribution of vibrational state population are predicted, particularly when vibrational energy is exchanged between two near-resonant diatomic species. Radiative gain coefficients for nonequilibrium vibration-rotation transitions are also computed and positive gains, sufficient to support laser oscillations, are predicted for CO-N2 and CO-N,-Ar admixtures.

Official Gazette of the United States Patent Office
  • Language: en
  • Pages: 1846

Official Gazette of the United States Patent Office

  • Type: Book
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  • Published: 1974
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  • Publisher: Unknown

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