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Thursday, May 7, 2020 | History

3 edition of Key topics for high-lift research found in the catalog.

Key topics for high-lift research

David Fisher

Key topics for high-lift research

a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996

by David Fisher

  • 100 Want to read
  • 31 Currently reading

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

    Subjects:
  • Flight tests.,
  • Wind tunnel tests.,
  • Flow distribution.,
  • Fins.,
  • Airfoils.,
  • Aerodynamics.,
  • F-15 aircraft.,
  • Lift.

  • Edition Notes

    Other titlesKey topics for high lift research., Joint wind tunnel/flight test approach.
    Statementcollaborators: David Fisher, Flint O. Thomas, and Robert C. Nelson.
    Series[NASA contractor report] -- NASA-CR-202525., NASA contractor report -- NASA CR-202525.
    ContributionsThomas, Flint O., Nelson, Robert C., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18116300M

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    per hour and a long test section adapted for high-lift research. The first test section is equipped with a six-component motorized pitch-and-yaw balance system. Instrumentation includes a two-component laser Doppler velocimeter system and a computer data acquisition system. Three smaller low-speed wind tunnels are also located at ASL. One has. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods.

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Key topics for high-lift research by David Fisher Download PDF EPUB FB2

Key Topics for High-Lift Research: A Joint Wind Tunnel / Flight Test Approach ///, ,i,_ 'ii_ 0 _" iREPORT for NASA-Ames University Consortium Joint Research Interchange May 1, - Septem COLLABORATORS David Fisher NASA Dryden Flight Research Center Flint O. Thomas Associate Professor, and Robert C.

Nelson Professor File Size: 1MB. The complex flow field over any multi-element airfoil may be broken down into certain generic component flows which are termed high-lift building block flows. In this report a broad spectrum of key flow field physics issues relevant to the design of improved high lift systems are considered.

Get this from a library. Key topics for high-lift research: a joint wind tunnel/flight test approach: report for NASA-Ames University consortium, joint research interchange, May 1, - Septem [David F Fisher; Flint O Thomas; Robert C Nelson; United States.

National Aeronautics and Space Administration.]. Finally, this book is a good reference for graduate students and researchers interested in the field of simulation of high-lift configurations. Discover the world's research 16+ million members.

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