Second-Order Shock-Expansion Theory Extended to Include Real Gas Effects

reportActive / Technical Report | Accession Number: ADA247191 | Open PDF

Abstract:

New methods have been developed to compute inviscid surface pressures and temperatures for both perfect and equilibrium chemically reacting flows on both pointed and blunt bodies of revolution. These new methods include an improved Shock-expansion Theory, an improved Modified Newtonian Theory MNT, and an improved method for angle-of-attack effects. Comparison of these approximate engineering techniques to exact inviscid computations using a full Euler code showed that these new methods gave very good agreement of surface temperature and pressures as well as forces and moments. Incorporation of this new technology into the NAVSWC aeroprediction code will allow the code to be used for engineering estimates of inviscid surface temperature at high Mach numbers. These approximate temperatures can then be used as inputs to perform heat transfer analysis. Second-order Shock-expansion, Perfect and Real Gases, Modified Newtonian Theory, Chemical Species Composition.

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