A primitive variable mathematical model for predicting the flows in turbojet test cells
by Stevenson, Charles A.
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An adaptation of a primitive variable, finite-difference computer program was made in order to predict the non-reacting flow fields in turbojet test cells. The study compares the predictions of the primitive variable computer model with an earlier stream function-vorticity computer model and empirical data. It was found that the model reasonably predicted the flow fields and allowed simulation of test cell flows up to full engine throttle conditions.
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Airplanes, Testing, Turbojet engines, Fluid dynamics, Mathematical modelsShowing 1 featured edition. View all 1 editions?
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A primitive variable mathematical model for predicting the flows in turbojet test cells
1979, Naval Postgraduate School
in English
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Edition Notes
"NPS67-79-009"--Cover.
"October 1979"--Cover.
Title from cover.
"Prepared for: Naval Air Propulsion Center, Trenton, NJ."
Includes bibliographical references (p. 42-43).
"Approved for public release; distribution is unlimited"--Cover.
Technical report; 1979.
ck/ 6/10/09.
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