The Control Volume Concept in Aeronautical Engineering.

Abstract

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.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1971
Accession Number
AD0741132

Entities

People

  • Carlos Tromben Corbalan

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Continuity
  • Engineering

Fields of Study

  • Physics

Readers

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  • Technical Research and Report Writing.