Last edited by Visho
Friday, April 17, 2020 | History

3 edition of An analysis for high Reynolds number inviscid/viscid interactions in cascades found in the catalog.

An analysis for high Reynolds number inviscid/viscid interactions in cascades

Mark Barnett

An analysis for high Reynolds number inviscid/viscid interactions in cascades

  • 245 Want to read
  • 0 Currently reading

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

    Subjects:
  • Aerodynamics.

  • Edition Notes

    StatementMark Barnett, Joseph M. Verdon, and Timothy C. Ayer.
    Series[NASA contractor report] -- NASA CR-4519., NASA contractor report -- NASA CR-4519.
    ContributionsVerdon, Joseph M., Ayer, Timothy C., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14707409M


Share this book
You might also like
Secondary school case studies

Secondary school case studies

Strategic bombers

Strategic bombers

Hymns, composed by different authors, by order of the General Convention of Universalists of the New-England states and others

Hymns, composed by different authors, by order of the General Convention of Universalists of the New-England states and others

Derivations

Derivations

Coast Guard Authorization Act of 1984

Coast Guard Authorization Act of 1984

A present ansvver to the late complaint unto the House of Commons. By divers members of the said House

A present ansvver to the late complaint unto the House of Commons. By divers members of the said House

The Pennsylvania, New-Jersey, Delaware, Maryland, and Virginia almanac, for the year of our Lord, 1805 ...

The Pennsylvania, New-Jersey, Delaware, Maryland, and Virginia almanac, for the year of our Lord, 1805 ...

The radical center

The radical center

Vegetarian Cooking for Beginners

Vegetarian Cooking for Beginners

Aquifer vulnerability analysis using the pesticide root-zone model (PRZM2)

Aquifer vulnerability analysis using the pesticide root-zone model (PRZM2)

Catholic art education: the new trends

Catholic art education: the new trends

The capns wife

The capns wife

An analysis for high Reynolds number inviscid/viscid interactions in cascades by Mark Barnett Download PDF EPUB FB2

Get this from a library. An analysis for high Reynolds number inviscid/viscid interactions in cascades. [Mark Barnett; Joseph M Verdon; Timothy C Ayer; United States. National Aeronautics and. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Analysis of High Reynolds Number Inviscid/ Viscid Interactions in Cascades J Thrust Imparted to an Airfoil by Passage Through a Sinusoidal Upwash Field J Prismatic Grid Generation for Three-Dimension-al Complex Geometries J Observations of Liquid Jets Injected into a High-ly Accelerated Supersonic Boundary Layer JAn analysis for high Reynolds number inviscid/viscid interactions in cascades book of aerodynamics: bases of aerodynamic design / Arnold M.

Kuethe, Chuen-Yen Chow Wiley New York Wikipedia Citation Please see Wikipedia's template documentation for further citation fields that may be required. Abstract. A recently developed nonlinear, compressible viscous-layer analysis and code has been extended and coupled to a linearized inviscid aerodynamic analysis to predict high Reynolds number subsonic unsteady flows through isolated, two-dimensional blade by: 1.

This banner text can have markup. web; books; video; audio; software; images; Toggle navigation. Thus, high Reynolds number flows driven by small amplitude unsteady excitations have been considered. The resulting analyses should apply in many practical situations and lead to a better.

An efficient analysis for predicting steady, inviscid-viscid interaction phenomena, such as viscous-layer separation, shock/boundary-layer interaction, and trailing-edge/near-wake interaction, in. The leading-edge flaps were deflected 4 deg to 15 deg, and the trailing-edge flaps were deflected from deg to 10 deg.

Longitudinal force and moment data were obtained at Mach numbers of,and for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of x 10(exp 6) per foot and for an angle-of-attack range 4.