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Monday, May 4, 2020 | History

3 edition of Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft found in the catalog.

Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft

Jack G. McArdle

Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft

  • 9 Want to read
  • 5 Currently reading

Published by National Aeronautics and Space Administration, For sale by the National Technical Information Service in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Supersonic nozzles.

  • Edition Notes

    StatementJack G. McArdle and Barbara S. Esker and James A. Rhodes.
    SeriesNASA technical memorandum -- 105698., NASA technical memorandum -- 105698.
    ContributionsEsker, Barbara S., Rhodes, James A. 1909-2001., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17786057M

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Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft by Jack G. McArdle Download PDF EPUB FB2

Get this from a library. Internal reversing Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft book in a tailpipe offtake configuration for SSTOVL aircraft. [Jack G McArdle; Barbara S Esker; James A Rhodes; United States.

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A system, method, and apparatus for throat corner scoop offtake for mixed compression inlets for high speed aircraft engine applications is disclosed. The throat corner scoops are small air intakes located inside the large mixed compression inlet.

They are positioned in a region otherwise prone to generate low pressure airflow. The throat corner scoops capture and remove the low pressure Cited by: 9.

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The flow is switched by means of a high temperature resistant cast iron sliding Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft book. The door movement is vertical and driven by a reversible electric gear motor. The door movement is vertical and driven by a reversible electric gear motor.

Tubular-type designs are generally considered one of the most promising devices for commercialization due to their stable structure without a high-temperature sealing anode support T-SOFC units are adopted to construct the stack (Fig. 1a), it is quite difficult to determine a proper external air flow path design to satisfy the high air flow distribution qualities on two Cited by: internal flows.

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air flowing around fuselage mixing with air flowing around an external fuel tank – we know drag of the fuselage and fuel tank individually – total drag after attaching fuel tank will be greater than the sum of the fuselage and fuel tank separately • Causes eddy currents, restrictions, and turbulence to smooth flow • Varies directly with the airspeed.

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