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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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a unique spectroscopic signature of concerted intermolecular charge shifts. NBO analysis suggests how the nonlinear cooperativity<br />

effects can be rationalized in terms of the fundamental n(sub N) yields sigma(sup *, sub CH) ”charge transfer” (”resonance”)<br />

nature of H bonding, manifested even in low-polarity H bonds involving CH groups.<br />

Author<br />

Infrared Spectroscopy; Hydrocyanic Acid; Dielectric Properties; Structural Analysis<br />

<strong>2000</strong>0065620 NASA Marshall Space Flight Center, Huntsville, AL USA<br />

Thermophysics Characterization of Kerosene Combustion<br />

Wang, Ten-See, NASA Marshall Space Flight Center, USA; [<strong>2000</strong>]; 31p; In English; 34th; Thermophysics, 19-22 Jun. <strong>2000</strong>, Denver,<br />

CO, USA; Sponsored by American Inst. of Aeronautics <strong>and</strong> Astronautics, USA; Original contains color illustrations; Copyright<br />

Waived; Avail: CASI; A03, Hardcopy; A01, Microfiche<br />

A one-formula surrogate fuel formulation <strong>and</strong> its quasi-global combustion kinetics model are developed to support the design<br />

of injectors <strong>and</strong> thrust chambers of kerosene-fueled rocket engines. This surrogate fuel model depicts a fuel blend that properly<br />

represents the general physical <strong>and</strong> chemical properties of kerosene. The accompanying gaseous-phase thermodynamics of the<br />

surrogate fuel is anchored with the heat of formation of kerosene <strong>and</strong> verified by comparing a series of one-dimensional rocket<br />

thrust chamber calculations. The quasi-global combustion kinetics model consists of several global steps for parent fuel decomposition,<br />

soot formation, <strong>and</strong> soot oxidation, <strong>and</strong> a detailed wet-CO mechanism. The final thermophysics formulations are incorporated<br />

with a computational fluid dynamics model for prediction of the combustor efficiency of an uni-element, tri-propellant<br />

combustor <strong>and</strong> the radiation of a kerosene-fueled thruster plume. The model predictions agreed reasonably well with those of the<br />

tests.<br />

Author<br />

Combustion Physics; Computational Fluid Dynamics; Kerosene; Mathematical Models; Rocket Engine Design; Reaction Kinetics;<br />

Thermodynamics<br />

<strong>2000</strong>0065632 NASA Marshall Space Flight Center, Huntsville, AL USA<br />

Parallel Processing in Combustion Analysis<br />

Schunk, Richard Gregory, NASA Marshall Space Flight Center, USA; Chung, T. J., Alabama Univ., USA; Apr. 26, <strong>2000</strong>; 19p;<br />

In English; Finite Elements in Flow Problems, 30 Apr. - 4 May <strong>2000</strong>, Austin, TX, USA; No Copyright; Avail: CASI; A03, Hardcopy;<br />

A01, Microfiche<br />

The objective of this research is to demonstrate the application of the Flow-field Dependent Variation (FDV) method to a<br />

problem of current interest in supersonic chemical combustion. Due in part to the stiffness of the chemical reactions, the solution<br />

of such problems on unstructured three dimensional grids often dictates the use of parallel computers. Preliminary results for the<br />

injection of a supersonic hydrogen stream into vitiated air are presented.<br />

Derived from text<br />

Flow Distribution; Parallel Processing (Computers); Supersonic Combustion; Parallel Computers<br />

<strong>2000</strong>0065650 Wisconsin Univ., Dept. of Chemistry, Madison, WI USA<br />

Quadrupole Coupling Constants in Linear (HCN(n) Clusters: Theoretical <strong>and</strong> Experimental Evidence for Cooperativity<br />

Effects in C-H...N Hydrogen Bonding<br />

King, B. F., Wisconsin Univ., USA; Farrar, T. C., Wisconsin Univ., USA; Weinhold, F., Wisconsin Univ., USA; Journal of Chemical<br />

Physics; Jul. 01, 1995; ISSN 0021-9606; <strong>Volume</strong> 103, No. 1, pp. 348-352; In English<br />

Contract(s)/Grant(s): NSF CHE-90-07850; NSF CHE-91-02674; Copyright; Avail: Issuing Activity<br />

Ab initio quadrupole coupling constants chi(D), chi(N-14) for deuterium <strong>and</strong> nitrogen nuclei are obtained for the sequence<br />

of linear (HCN)(n) clusters (up to n=6) at the RHF/6-31 + G* level, complementing previous studies of n-dependent ”cooperative”<br />

effects in these C-H ... N hydrogen-bonded species. For the dimer <strong>and</strong> trimer, the theoretical values are compared with experimental<br />

equilibrium values of Gutowsky <strong>and</strong> co-workers <strong>and</strong> found to successfully reproduce both the magnitudes <strong>and</strong> patterns of measured<br />

shifts. For larger (HCN)(n) clusters, the n-dependent trends in chi(D), chi(N-14) appear to be correlated with cooperativity<br />

effects found previously (binding energies, geometrical parameters, dipole moments, ir frequencies <strong>and</strong> intensities). This suggests<br />

that quadrupole coupling measurements can provide a useful probe of cooperative H-bonding phenomena in gaseous <strong>and</strong> condensed<br />

media.<br />

Author<br />

Quadrupoles; Coupling; Constants; Molecular Clusters; Hydrocyanic Acid<br />

48

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