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Wednesday, July 29, 2020 | History

3 edition of Assessment of dual-point drag reduction for an executive-jet modified airfoil section found in the catalog.

Assessment of dual-point drag reduction for an executive-jet modified airfoil section

Assessment of dual-point drag reduction for an executive-jet modified airfoil section

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Airfoil profiles.,
  • Angle of attack.,
  • Boundary layer transition.,
  • Drag reduction.,
  • Force distribution.,
  • Pitching moments.,
  • Reynolds number.,
  • Trailing edges.,
  • Transonic wind tunnels.,
  • Aerodynamic characteristics.

  • Edition Notes

    Other titlesAssessment of dual point drag reduction for an executive-jet modified airfoil section.
    StatementDennis O. Allison and Raymond E. Mineck.
    SeriesNASA technical paper -- 3579.
    ContributionsMineck, Raymond E., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15504416M


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Assessment of dual-point drag reduction for an executive-jet modified airfoil section Download PDF EPUB FB2

Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section Dennis 0. Allison and Raymond E. Mineck Langley Research Center • Hampton, Virginia National Aeronautics and Space Administration Langley Research Center • Hampton, Virginia July Assessment of dual-point drag reduction for an executive-jet modified airfoil section (SuDoc NAS ) [Dennis O.

Allison] on *FREE* shipping on qualifying offers. Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section by National Aeronautics and Space Adm Nasa,available at Book.

Assessment of dual-point drag reduction for an executive-jet modified airfoil section | NASA, National Aeronautics and Space Administration | ISBN: | Kostenloser Versand für alle Bücher mit Versand und Verkauf duch : Taschenbuch. Get this from a library. Assessment of dual-point drag reduction for an executive-jet modified airfoil section.

[Dennis O Allison; Raymond E Mineck; Langley Research Center.]. Assessment of dual-point drag reduction for an executive-jet modified airfoil section. Hampton, Va.: [Springfield, Va: National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor.

MLA Citation. Allison, Dennis O. and Mineck, Raymond E. and Langley Research Center. Assessment of dual-point drag reduction for an executive-jet modified airfoil section eBook: National Aeronautics and Space Administration NASA: : Kindle Store. Buy Assessment of dual-point drag reduction for an executive-jet modified airfoil section (SuDoc NAS ) by Dennis O.

Allison (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Dennis O. Allison. {{Citation | title=Robust airfoil optimization to achieve consistent drag reduction over a mach range [microform] / Wu Li, Luc Huyse, Sharon Padula | author1=Li, Wu | author2=Huyse, Luc | author3=Padula, Sharon | author4=Langley Research Center | year= | publisher=National Aeronautics and Space Administration, Langley Research Center.

Noté /5. Retrouvez Assessment of dual-point drag reduction for an executive-jet modified airfoil section et des millions de livres en stock sur Achetez neuf ou d'occasionFormat: Broché. Achetez et téléchargez ebook Assessment of dual-point drag reduction for an executive-jet modified airfoil section (English Edition): Boutique Kindle - Science: at: Format Kindle.

Assessment of dual-point drag reduction for an executive-jet modified airfoil section (English Edition) eBook: National Aeronautics and Space Administration NASA: : Kindle-ShopFormat: Kindle. Dennis O. Allison and Raymond E.

Mineck, Aerodynamic Characteristics and Pressure Distributions for an Executive-Jet Baseline Airfoil Section, NASA TM, Decemberpp.

The paper is missing figures. Please see of the Frequently Asked Questions (FAQ) for information on how to obtain a hardcopy of this document.

Effect of Full-Chord Porosity on Aerodynamic Characteristics of the NACA Airfoil. NASA Technical Reports Server (NTRS) Mineck, Raymond E.; Hartwich, Peter M. A te. Statistical Analysis of the AIAA Drag Prediction Workshop CFD Solutions. NASA Technical Reports Server (NTRS) Morrison, Joseph H.; Hemsch, Michael J.

The first AIAA Dr. The high-aspectratio airfoil has a rectangular center section and double-taper outer panels with 2V2C dihedral.

Two sections of doubleslotted flaps line the trailing edge inboard of the ailerons; two sections of spoilers fitted ahead of the outer flap sections assist in roll control and are used as lift dumpers. This banner text can have markup.

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