Accession Number:

AD0736310

Title:

Inlets and Nozzles for Aerospace Engines

Descriptive Note:

Conference proceedings no. 91

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1971-12-01

Pagination or Media Count:

503.0

Abstract:

Contents Engine-airplane interference representation in wind tunnel testing Thrust vectoring and control Vstol inlets and nozzles Supersonic inlets, nozzles, and applications Subsonic and transonic aeropropulsion.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE