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An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Scott, Carl D. Brykina, Irina G. |
| Copyright Year | 1998 |
| Description | A technique is implemented for computing hypersonic aeroheating, shear stress, and other flow properties on the windward side of a three-dimensional (3D) blunt body. The technique uses a 2D/axisymmetric flow solver modified by scale factors for a, corresponding equivalent axisymmetric body. Examples are given in which a 2D solver is used to calculate the flow at selected meridional planes on elliptic paraboloids in reentry flight. The report describes the equations and the codes used to convert the body surface parameters into input used to scale the 2D viscous shock layer equations in the axisymmetric viscous shock layer code. Very good agreement is obtained with solutions to finite rate chemistry 3D thin viscous shock layer equations for a finite rate catalytic body. |
| File Size | 1046412 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980151085 |
| Archival Resource Key | ark:/13960/t01z94m2v |
| Language | English |
| Publisher Date | 1998-05-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Three Dimensional Bodies Shock Layers Flow Coefficients Hypersonics Aerodynamic Heating Flow Measurement Shear Stress Flow Characteristics Blunt Bodies Parabolic Bodies Axisymmetric Bodies Axisymmetric Flow 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 |
