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Sunday, August 9, 2020 | History

2 edition of More tests with a variable ramp intake having a design mach number of 2.2 found in the catalog.

More tests with a variable ramp intake having a design mach number of 2.2

M. C. Neale

More tests with a variable ramp intake having a design mach number of 2.2

by M. C. Neale

  • 77 Want to read
  • 11 Currently reading

Published by H.M.S.O. in London .
Written in English

    Subjects:
  • Airplanes -- Jet propulsion -- Air intakes.

  • Edition Notes

    Statementby M. C. Neale and P. S. Lamb.
    SeriesAeronautical Research Council. Current papers,, no. 938, Current papers (Aeronautical Research Council (Great Britain)) ;, no. 938.
    ContributionsLamb, P. S., joint author.
    Classifications
    LC ClassificationsL507 .G77 no. 938
    The Physical Object
    Pagination16 p.
    Number of Pages16
    ID Numbers
    Open LibraryOL5588308M
    LC Control Number67108722
    OCLC/WorldCa6163430

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More tests with a variable ramp intake having a design mach number of 2.2 by M. C. Neale Download PDF EPUB FB2

More tests mlth a variable ramp intake having a design Mach number of - by - M. Neale and P. Lamb SUMMARY Results are repvted of tests on a two-dimensional combined external/internal compressIon Intake having a design Mach number of File Size: 2MB.

Tests with a variable ramp intake having combined external/internal compression, and a design Mach number of - by - M. Neale and P. Lamb August, Results are reported of tests on a two-dimensional combined external/internal compression intake having a.

" Some Test with Variable Ramp Intake Having Combined External/Internal Compression, and a Design Mach Number of" Aeronautical Research Council. A variable-sweep wing, colloquially known as a "swing wing", is an airplane wing, or set of wings, that may be swept back and then returned to its original straight position during allows the aircraft's shape to be modified in flight, and is therefore an example of a variable-geometry aircraft.

A straight wing is most efficient for low-speed flight, but for an aircraft designed for. May Design And Development of a Variable Geometry Intake for a 4-Stroke 4 Cylinder Engine Wasim Sarwar - Supervisor: Dr.

Iain Dupère When optimizing a. More Tests with a Variable Ramp Intake Having a Design Mach Number ofAeronautical Research Council, London, PRELIMINARY INVESTIGATION OF SUPERSONIC DIFFUSERS Article.

The Panavia Tornado is a family of twin-engine, variable-sweep wing multirole combat aircraft, jointly developed and manufactured by Italy, the United Kingdom, and West are three primary Tornado variants: the Tornado IDS (interdictor/strike) fighter-bomber, the suppression of enemy air defences Tornado ECR (electronic combat/reconnaissance) and the Manufacturer: Panavia Aircraft GmbH.

The Rolls-Royce/SNECMA Olympus (which powered the Concorde) used a complex intake-ramp system to improve the engine's efficiency and prevent an engine shutdown or failure during supersonic flight. 45, ft at a freestream Mach number ofand with an over-wing Mach number of Two similar inlet designs were tested experimentally in the 8.

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A rectangular stream-tube stream-traced Busemann intake, shown in Fig. 27, for a design Mach number was tested in Mach and Mach wind tunnels to investigate the overall performance. To obtain off-design performance data the model shape was based on Mach Busemann flow and the leading edge was truncated at a surface angle of 6 Cited by: 1.

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• The attainment of high performance is generally more difficult in those regions requiring a rise. A variable-sweep wing, colloquially known as a "swing wing", is an airplane wing, or set of wings, that may be swept back and then returned to its original position during allows the aircraft's shape to be modified in flight, and is therefore an example of a variable-geometry aircraft.

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