Sabtu, 06 November 2010

A Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber Pdf

A Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber
Author: Mehmet Koray Savur
Edition:
Binding: Kindle Edition
ISBN: B007E3FTM0

A numerical study was conducted to predict the combined convective and radiative heat transfer rates on the walls of a small aspect ratio cylinder representative of the scaled model of a rocket engine combustion chamber. Download A Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber from rapidshare, mediafire, 4shared. A high-temperature, high-pressure environment was simulated in the cylinder, with gas velocities at low subsonic levels typical of the conditions leading to the entrance of the nozzle section of a rocket engine. The composition of the gases in the cylinder was determined from the TEP program for the burning of rocket fuel at typical values of the O/F ratio. The thrust of the study was to determine the radiative contribution to the heat transfer rate from the hot participating chamber gases to the cooler wall. The calculations Search and find a lot of medical books in many category availabe for free download. A Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber medical books pdf for free. The calculations



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