Accession Number:

AD0701115

Title:

SUPERSONIC TURBO-JET PROPULSION SYSTEMS AND COMPONENTS,

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

• Chauvin, J.

Report Date:

1969-01-01

Pagination or Media Count:

483.0

Abstract:

Contents Supersonic inlets Supersonic compressors Supersonic combustion technology Air cooling of turbine blades and vanes Exhaust nozzles A survey of fluidic components and their application to gas turbine control and Interface problems of high speed air-breathing airplane engines.

Descriptors:

• *SYMPOSIA
• *SUPERSONIC COMBUSTION RAMJET ENGINES
• *TURBOJET ENGINES
• CONTROL SYSTEMS
• INTERFACES
• AIR COOLED
• AXIAL FLOW COMPRESSORS
• TURBOJET EXHAUST NOZZLES
• FLUID AMPLIFIERS
• FLUIDICS
• TURBOJET INLETS
• SUPERSONIC COMBUSTION
• SUPERSONIC CHARACTERISTICS
• GAS TURBINE BLADES

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE