Accession Number:

ADA023471

Title:

Can-Type Combustor Design for a Low Cost Subsonic Ramjet Engine

Descriptive Note:

Final technical rept. 1 Apr 1974-1 Apr 1975

Corporate Author:

AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1975-12-01

Pagination or Media Count:

83.0

Abstract:

This study investigates the feasibility of using a low cost can combustor in a subsonic ramjet engine in the flight envelope of Mach 0.7 to 0.9, altitude 20,000 to 30,000 feet. A simple can combustor without close fabrication tolerances was designed and fabricated. The can was installed in a subsonic ramjet which was ground tested in a direct-connect pipe set-up. The combustion efficiency and thrust were determined at conditions representative of the flight envelope. These results are compared with results of a model subsonic ramjet engine cycle analysis. The end result of the program is a developed combustor system for a subsonic ramjet which is an inexpensive and attractive propulsion device for one-mission remotely piloted vehicles and target drones.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE