Space Shuttle laminar heating with finite-rate catalytic recombination
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- Calculation of metric coefficients for streamline coordinates.AIAA Journal, 1972
- On Catalytic Recombination Rates in Hypersonic Stagnation Heat TransferJournal of Jet Propulsion, 1958
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958