Propellant vaporization as a criterion for rocket engine design : relation between percentage of propellant vaporized and engine performance
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Heidmann, Marcus F↗
Engineering topics
Heidmann, Marcus F
Publications and source records attributed to Heidmann, Marcus F.
A Study of Sprays Formed by Two Impinging Jets
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Heidmann, Marcus F↗
Injection Principles for Liquid Oxygen and Heptane Using Two-element Injectors
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Heidmann, Marcus F↗
Fluctuations in a Spray Formed by Two Impinging Jets
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COMBUSTION - EFFECTS OF FUEL ATOMIZATION↗
Analysis of effect of variations in primary variables on time constant and turbine-inlet-temperature overshoot of turbojet engine
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TURBINES, GAS - TEMPERATURE↗
Method of determining conditions of maximum efficiency of an independent turbine-propeller combination
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GENERATORS, GAS↗
Control considerations for optimum power proportionment in turbine-propeller engines
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NOZZLES, EXHAUST - VARIABLE↗