Rocket Performance Prediction Technique
| Autor: | J. H. Morgenthaler, W. R. Stepien |
|---|---|
| Rok vydání: | 1975 |
| Předmět: |
business.product_category
business.industry Rocket engine nozzle Aerospace Engineering Mechanics Characteristic velocity Combustion Physics::Fluid Dynamics Rocket Space and Planetary Science Performance prediction Specific impulse Physics::Chemical Physics Diffusion (business) Combustion chamber Aerospace engineering business Mathematics |
| Zdroj: | Journal of Spacecraft and Rockets. 12:199-204 |
| ISSN: | 1533-6794 0022-4650 |
| DOI: | 10.2514/3.56964 |
| Popis: | Attention is given to a semiempirical correlation technique based on the rational assumption that the turbulent mixing of reactants is the rate controlling process in combustors employing diffusion flames. Questions of performance computation are considered along with the flow conditions. Predictions of combustion efficiency are obtained with the aid of a standard finite-difference computational technique. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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