Union Catalogue of Belgian Libraries
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Air intake problems in supersonic propulsion

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Infiltration and ventilation
Author:
Nylund, Per-Olof
ISBN: 915403275X
Year: 1980
Publisher: Stockholm : Swedish council for building research,

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Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets

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Investigation of flow fields within large-scale hypersonic inlet models

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Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients

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Experimental dynamic response of a two-dimensional, Mach 2.7, mixed-compression inlet

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Tests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.65

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Characteristics study of a bicone mixed-compression inlet for Mach 1.80 to 2.50

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Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack

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Air intake problems in supersonic propulsion : invited papers presented at the 11th AGARD combustion and propulsion panel meeting, Paris, December 1956
Author:
Fabri, Jean
Year: 1958
Publisher: London : Pergamon Press,

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