Accession Number : ADA116584

Title :   A Method for Designing Inlet Distortion Screens for Aircraft Gas Turbine Engine Tests Using an Interactive Computer Program.

Descriptive Note : Final rept.,

Corporate Author : NAVAL AIR PROPULSION CENTER TRENTON NJ PROPULSION TECHNOLOGY AND PROJECT ENGINEERING DEPT

Personal Author(s) : Anderson,Robert E

PDF Url : ADA116584

Report Date : May 1982

Pagination or Media Count : 35

Abstract : The design of inlet distortion screens used for testing aircraft gas turbine engines can be facilitated by using an interactive computer program. This report describes a computer program which has been developed by the Naval Air Propulsion Center to aid in the screen design process. The computer program can be used to establish the initial screen design and to develop modifications after the screen is tested. (Author)

Descriptors :   *Turbojet inlet screens, *Jet engine inlets, *Computer aided design, Distortion, Computer programs, Computer files, Methodology, Aircraft engines, Gas turbines

Subject Categories : Aircraft
      Computer Programming and Software
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE