Download PDF by Brian J. Cantwell: Aircraft and Rocket Propulsion

By Brian J. Cantwell

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Extra info for Aircraft and Rocket Propulsion

Example text

The goal of the designer is to produce a compression system that is as near to isentropic as possible. Station 4 - The exit of the burner. 56) The temperature at the exit of the burner is regarded as the highest temperature in the Brayton cycle although generally higher temperatures do occur at the upstream end of the burner where combustion takes place. The burner is designed to allow an influx of cooler compressor air to mix with the combustion gases bringing the temperature down to a level that the high pressure turbine can tolerate.

The goal of the designer is to produce a compression system that is as near to isentropic as possible. Station 4 - The exit of the burner. 56) The temperature at the exit of the burner is regarded as the highest temperature in the Brayton cycle although generally higher temperatures do occur at the upstream end of the burner where combustion takes place. The burner is designed to allow an influx of cooler compressor air to mix with the combustion gases bringing the temperature down to a level that the high pressure turbine can tolerate.

Station 4 - The exit of the burner. 56) The temperature at the exit of the burner is regarded as the highest temperature in the Brayton cycle although generally higher temperatures do occur at the upstream end of the burner where combustion takes place. The burner is designed to allow an influx of cooler compressor air to mix with the combustion gases bringing the temperature down to a level that the high pressure turbine can tolerate. Modern engines operate at values of T t4 that approach 3700°R (2050°K).

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Aircraft and Rocket Propulsion by Brian J. Cantwell


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