MODEL SCALING RULES FOR TURBOJET AND GAS TURBINE COMBUSTION CHAMBERS
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 02, 1968
- Accession Number
- AD0683222
Entities
People
- Ch'en Tan-shih
Organizations
- National Air and Space Intelligence Center