Aerodynamics of Power Plant Installation, Part I

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Aerodynamics of Power Plant Installation, Part I

Contents: Engine designer's 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.