NDLI: Computational fluid dynamics and aerothermodynamics

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Computational fluid dynamics and aerothermodynamics

Content Provider	NASA Technical Reports Server (NTRS)
Author	Carlson, Leland A.
Copyright Year	1988
Description	Approximations applicable to the radiating, reacting, and conducting stagnation region of a hypervelocity vehicle were incorporated into a method for rapidly obtaining approximate solutions. This solution utilizes a coordinate system based upon the origin of the radiative losses and includes in a phenomenologically correct manner the effects of chemical and thermal nonequilibrium, and nonequilibrium, nongray radiative transfer. Results were presented which demonstrate the usefulness of the method and indicate which radiation parameters require further study and definition. Excellent comparisons were obtained with published results for the Fire2 data. An axisymmetric nonequilibrium inverse method was modified and extended and used to investigate and compare various vibration dissociation chemistry coupling models and radiative heat transfer approximations. The similarities, differences, and consequences of using these models in the Aero-assist Orbital Transfer Vehicles flight regime will be discussed.
File Size	1722049
Page Count	54
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19880007605
Archival Resource Key	ark:/13960/t1jh8fn04
Language	English
Publisher Date	1988-03-01
Access Restriction	Open
Subject Keyword	Fluid Mechanics And Heat Transfer Orbit Transfer Vehicles Wings Vibration Computational Fluid Dynamics Reaction Kinetics Flow Distribution Stagnation Point Mathematical Models Aircraft Design Dissociation Radiative Heat Transfer Aerothermodynamics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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