FLOW OF GAS-PARTICLE MIXTURES IN AXIALLY SYMMETRIC NOZZLES
Abstract
Studies were made of one-dimensional gas-particle nozzle flows in axially symmetric nozzle. Comparisons between calculated and experimentally measured nozzle efficiencies are given for a metallized double base propellant whose exhaust contains 38% condensed oxides. It is shown that the theory predicts the performance of this propellant in nozzles of greatly different size, shape and expansion ratio, within the limits of the experimental measurements. It is concluded that the theory adequately describes the flow of gas-particle mixtures in axially symmetric nozzles.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1943
- Accession Number
- AD0422122
Entities
People
- Gary R. Nickerson
- James R. Kliegel