Accession Number:

AD0672073

Title:

INTEGRATION OF PROPULSION SYSTEMS IN AIRFRAMES

Descriptive Note:

Conference proceedings

Corporate Author:

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

Personal Author(s):

Report Date:

1967-09-01

Pagination or Media Count:

235.0

Abstract:

Contents The influence of flight speed on the thrust calibration of a jet engine Jet influence on VSTOL-aircraft in the transitional and high speed flight regime Some studies into improvements in automatic throttle control Engine airframe integration problems peculiar to aircraft configurations with nacelles mounted above the wing Aircraft and propulsion operational considerations related to inlet design A discussion of the use of thrust for control of VTOL aircraft Reaction control system preliminary design considerations for a jet-lift research aircraft Hot-gas ingestion and jet interference effects for jet VSTOL aircraft Interaction between airframe- powerplant integration and hot gas ingestion for jet lift VSTOL transport aircraft.

Descriptors:

• *JET ENGINES
• AIRCRAFT ENGINES
• AIRFRAMES
• DUCT INLETS
• INGESTION(ENGINES)
• JET FLOW
• LIFT
• NACELLES
• RESEARCH AIRCRAFT
• SYMPOSIA
• THROTTLING
• THRUST
• VERTICAL TAKEOFF AIRCRAFT

Subject Categories:

• VSTOL
• Research and Experimental Aircraft
• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE