A method for calculating axisymmetric afterbody flows
- 1 July 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 3 (4) , 357-364
- https://doi.org/10.2514/3.22998
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Results of AGARD assessment of prediction capabilities for nozzle afterbody flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The prediction of separated flow using a viscous-inviscid interaction methodThe Aeronautical Journal, 1985
- Theoretical analysis of aircraft afterbody flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Calculation of turbulent flow about missile afterbodies containing an exhaust jetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Viscous-inviscid interaction in transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical Simulation of Multistream Nozzle FlowsAIAA Journal, 1980
- Calculation of Separated Turbulent Flows on Axisymmetric Afterbodies Including Exhaust Plume EffectsAIAA Journal, 1980
- Matching Procedure for Viscous-Inviscid Interactive Calculations xAIAA Journal, 1979
- Approximation von Punktmengen durch implizite FunktionenZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1978
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954