Combustion in Liquid-Fuel Rocket Motors-Reference-Cited by-同舟云学术

Combustion in Liquid-Fuel Rocket Motors

Published:1959-02 Issue:1 Volume:10 Page:1-27
ISSN:0001-9259
Container-title:Aeronautical Quarterly
language:en
Short-container-title:Aeronautical Quarterly

Author:

Spalding D. B.

Abstract

SummaryThe paper provides a simplified picture of the processes occurring in liquid bi-propellant rocket motors. Droplet vaporisation, chemical reaction, and drag between gas and droplet are considered for a one-dimensional model. Quantitative theoretical results are presented for the variation of droplet size, droplet velocity, gas temperature and gas velocity within the chamber, particular attention being paid to the calculation of L*. The theory is applied to the German V2 rocket motor. Practical conclusions from, and extensions to, the theory are discussed.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference8 articles.

1. Saunders O. A. and Spalding D. B. Chemical and Physical Factors Controlling the Rats of Combustion. Joint Conference on Combustion, p. 14, Institution of Mechanical Engineers, 1955 (and other references given there).

2. Spalding D. B. and Jain V. K. Theory of the Burning of Mono-Propellant Droplets. A.R.C. 20,176, 1958.

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