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A theoretical calculation of the reduction in drag obtainable by ejector action of the exhaust gases when mixed with the cooling air-flow of a typical air-cooled engine
A. B. P. Beeton
(
1945
)
The increase in thrust obtainable from a power plant installation using the cooling-air as a propulsive jet
A. B. P. Beeton
(
1945
)
Part 1 Tabulated Thermal Data for Hydrocarbon Oxidation Products at High Temperatures. Part 2 The Effect of Dissociation on Rocket Performance Calculations
A. B. P. Beeton
(
1946
)
The calculated performance of ethyl alcohol-water mixtures as rocket fuels with liquid oxygen
A. B. P. Beeton
(
1948
)
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A. B. P. Beeton (4)
Date Issued
1948 (1)
1946 (1)
1945 (2)