MODEL SCALING RULES FOR TURBOJET AND GAS TURBINE COMBUSTION CHAMBERS
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
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Many rules for scaling turbojet and gas turbine combustion chambers have been developed in the past ten years, but none has been accepted as a general rule. This paper describes various methods in order to find possible scaling rules for such a combustion system. A scaling theory with respect to nonhomogeneous combustion of droplets under jet flow is suggested primarily to check various existing model scaling methods. On the basis of the suggested theory, the author finally proposes some new scaling rules and also offers conclusions for reference use in future studies.
- Combustion and Ignition