Application of near-equilibrium criteria during adiabatic flow to representative propellant systems
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering
Reference8 articles.
1. Adiabatic Flow of Hydrogen Gas through a Rocket Nozzle With and Without Composition Change;Penner;Journal Franklin Inst.,1948
2. Chemical Reactions During Adiabatic Flow Through a Rocket Nozzle;Altman;J. Chem. Phys.,1949
3. Maintenance of Near-Equilibrium during Isentropic Expansion through a Nozzle;Penner;J. Am. Chem. Soc.,1949
4. On the Thermodynamics of Rocket Propulsion, I;Schaefer,1947
5. Introduction to Quantum Mechanics;Pauling,1935
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Publications by S. S. Penner;Modern Developments in Energy, Combustion and Spectroscopy;1993
2. Exakte Berechnung der Leistung von Raketentreibstoffen;Raketentreibstoffe;1968
3. Nonequilibrium Expansions of Air with Coupled Chemical Reactions;Physics of Fluids;1962
4. Estimate of Chemical Space Heating Rates in Gas-Phase Combustion With Application to Rocket Propellants;ARS Journal;1960-02
5. DISCUSSIONS;The Chemistry of Propellants;1960
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