Reisch, U. and Streit, Th. (1996) Surface Inclination and Heat Transfer Methods for Reacting Hypersonic Flow in Thermochemical Equilibrium. DLR-Interner Bericht. 129-96/10, 34 S.
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For the design of hypersonic configurations heat transfer plays an essential role. At high velocities high-temperature effects have to be taken into account; here a perfect gas assumtion for air leads to major errors concerning the calculation of temperature and heat transfer. Therefore in this work the DLR design tool HOTSOSE is extended to applications for chemically reacting air in thermochemical equilibrium. Computations for various geometries including high-temperature effects were carried our to validate the HOTSOSE code. The results are compared to Euler- and Navier-Stokes-solutions, HOTSOSE perfect gas results and experimental data. For invicid flow, the pressure is calculated from surface inclinationmethods. The respective flow variables are obtained from isentropic relations for perfect gas using piecewise constant gas properties, or from the oblique shock relations, which are solved iteratively.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Surface Inclination and Heat Transfer Methods for Reacting Hypersonic Flow in Thermochemical Equilibrium|
|Number of Pages:||34|
|Keywords:||Aerothermodynamics, hypersonic flow, surface inclination methods, approx. heat transfer methods, reacting flow......|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||L - Military Technologies|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:06|
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