Computer Program for Calculation of Turbojet System Performance.

Abstract

A computer program has been written which calculates combined turbojet engine, air induction and exhaust system characteristics to produce integrated propulsion system performance.

Document Details

• Document Type: Technical Report
• Publication Date: Jun 15, 1982
• Accession Number: ADA120665

Entities

People

• Joseph J. Franz

Organizations

• Naval Air Warfare Center Warminster

Tags

DTIC Thesaurus Topics

• Computer Programs
• Computers
• Engineering
• Engines
• Exhaust Systems
• Jet Aircraft
• Mechanical Engineering
• Propulsion Systems
• Thermal Propulsion Systems
• Turbojet Engines

Fields of Study

• Physics

Readers

• Aerospace Engineering
• Computer Science.