Accession Number:

AD0656569

Title:

AERODYNAMICS OF POWER PLANT INSTALLATION, PART 1

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1965-10-01

Pagination or Media Count:

363.0

Abstract:

Contents Engine designers point of view A discussion of selected aerodynamic problems on integration of propulsion systems with airframe on transport aircraft The feasibility of supersonic combustion ramjets for low hypersonic speeds The blunt trailing edge axial-flow supersonic compressor Measurements of relaxation effects in nozzle flow of hot combustion gases by means of a shock tube technique Aircraft performance problems associated with engine and intake installation Low-drag installation of twin propulsion nozzles in the rear of the fuselage for transonic and supersonic flight Method of net thrust measurement in supersonic flight Past flight experience and recent developments in combinations of ramjet and turbojet engines Additive drag on inlet cowls and its effect on aircraft performance Intake design and performance around a Mach number of 2.2 Fonctionnement du piege a couche limite interne d une prise d air a compression supersonique externe A general method for calculating low speed flow about inlets.

Descriptors:

• *AIRCRAFT ENGINES
• AERODYNAMICS
• AIRCRAFT ENGINE DUCTS
• AXIAL FLOW COMPRESSORS
• DRAG
• EXHAUST GASES
• NATO
• NOZZLE GAS FLOW
• PERFORMANCE(ENGINEERING)
• RAMJET ENGINES
• SUPERSONIC COMBUSTION RAMJET ENGINES
• SUPERSONIC FLIGHT
• SYMPOSIA
• TRANSPORT AIRCRAFT
• TURBOJET ENGINES

Subject Categories:

• Transport Aircraft
• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE