Last edited by Fesida
Tuesday, April 28, 2020 | History

2 edition of Jet-induced ground effects on a parametric flat-plate model in hover found in the catalog.

Jet-induced ground effects on a parametric flat-plate model in hover

Jet-induced ground effects on a parametric flat-plate model in hover

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  • 10 Currently reading

Published by National Aeronautics and Space Administration, Ames Research Center, National Technical Information Service, distributor in Moffett Field, Calif, [Springfield, Va .
Written in English

    Subjects:
  • Aerodynamics.

  • Edition Notes

    Other titlesJet induced ground effects on a parametric ....
    StatementDouglas A. Wardwell ... [et al.].
    SeriesNASA technical memorandum -- 104001.
    ContributionsWardwell, Douglas A., Ames Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14698470M


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Jet-induced ground effects on a parametric flat-plate model in hover Download PDF EPUB FB2

Get this from a library. Jet-induced ground effects on a parametric flat-plate model in hover. [Douglas A Wardwell; Ames Research Center.;].

NPR effects were looked at, however, in an extensive study of jet-induced interference effects undertaken by Shumpert and Tibbetts. Tests were conducted on a 14 per cent scale model of a jet VTOL aircraft with a fuselage-mounted lift system at Jet-induced ground effects on a parametric flat-plate model in hover book ratios of, and Cited by: 2.

This paper provides a review of the out-of-ground-effect propulsion-induced interference on the aerodynamics of jet-lift short take-off and vertical landing (STOVL) aircraft. Twin Impinging Jets Through a Crossflow. lift jet VTOL aircraft operating in the hover mode in and out of ground effect.

effects of axisymmetric and flat plate geometries on the nature. Jet induced lift lose (2) Figure This is the general lift force trend found for our underwater robot. We broadly divided into 3 regions, (1) Pressure build up and leading to a large lift force (2) Suckdown or jet induced lift loss region (3) Fountain upwash or positive lift region.

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Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A continuing bibliography with indexes (supplement )" See other formats. Full text of "NASA Technical Reports Server (NTRS) Aeronautical Engineering: A continuing bibliography, cumulative index" See other formats.

A numerical procedure to predict the effects of Reynolds number and trip strip variation on three-dimensional wing lift and pitching moment R. LUH and M. MACK. You can write a book review and share your experiences. Other readers will always be interested in your opinion of the books you've read.

Whether you've loved the book or not, if you give your honest and detailed thoughts then people will find new books that are right for them. Full text of "NASA Technical Reports Server (NTRS) A cumulative index to Aeronautical Engineering: A continuing bibliography, supplement " See other formats.

7 Take-off and landing Definition of terminal phases Conventional take-off Ground run of jet aircraft Solutions of the take-off equation Rotation and initial climb Take-off with one engine inoperative Calculation of the balanced field length Ground run of propeller aircraft WAT charts Missed take-off 7.

Aerospace Engineering Desk Reference Note from the Publisher This book has been compiled using extracts from the following books within the range of Aerospace books in the Elsevier collection: Filippone () Flight Performance of Fixed and Rotary Aircraft Megson () Aircraft Structures for Engineering Students Cook () Flight Dynamics Principles.

Effects of varying jet decay rate on jet-induced loads on a flat plate located in the plane of the jet exit perpendicular to the jet axis were investigated using a small-scale laboratory facility.

Jet decay rate has been varied through use of two cylindrical centerbodies having either a flat or hemispherical tip, which were submerged various. This model extend two widely used models, the Kelvin-Helmholtz (KH) instability of Reitz (blob model) and the Taylor-Analogy-Breakup (TAB) secondary droplet breakup by O'Rourke and Amsden to include turbulence effects.

In the primary breakup model, the level of the turbulence effect on the liquid breakup depends on the characteristic scales and. The Ousterhout increase in its extent as the deflection angle was investigation used the same cm diameter jet in a decreased. The wake region showed a rapid pressure flat plate model and in a cm diameter circular body recovery for deflection angles of 30" or more.

Below a model. Template-Type: ReDIF-Paper Handle: NDLTD:VTETD::etd Title: Conceptual Development and Empirical Testing of an Outdoor Recreation Experience Model: The Recreat. % GENERAL CITATIONS @Book{panton, author = {Panton, R.

L.}, title = {Incompressible Flow}, publisher = {John Wiley and Sons}, year = {}, address = {New York.