The Control Volume Concept in Aeronautical Engineering.
NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF
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The thesis is concerned with the fundamental physical laws of continuity, momentum, and energy used in aeronautical engineering which are transformed from the control mass or system form into the control volume form. It is intended for the document to serve as a self-studying guide for students in the core of the aeronautical engineering program at the Naval Postgraduate School and as a reference during the graduate level courses.
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- Fluid Mechanics