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Input Data Description of the HOTSOSE Code

Eggers, T. (2002) Input Data Description of the HOTSOSE Code. DLR-Interner Bericht. IB 124-2002/22.

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This note describes the input and output files required for the application of HOTSOSE. The program computes the total aerodynamic coefficients and the surface flow variables using surface inclination methods and approximate methods to evaluate the heat transfer and skin friction coefficient for perfect gas or chemical reacting air in thermochemical equilibrium. With regard to the theory behind HOTSOSE, important general comments or reference calculations, references [1],[2],[3] have to be taken into account.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Input Data Description of the HOTSOSE Code
AuthorsInstitution or Email of Authors
Keywords:hypersonic flow, aerodynamic coefficients, surface inclination methods, approximate heat transfer and skinfriction methods
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:06

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