Supercritical flow

Results: 20



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11This model was tested in the 0.3m Transonic Cryogenic Tunnel ( Bldg[removed]in the[removed]timeframe. Two technologies were merging that inspired the contour of the airfoil. First, the LaRC LFC program (Laminar Flow C

This model was tested in the 0.3m Transonic Cryogenic Tunnel ( Bldg[removed]in the[removed]timeframe. Two technologies were merging that inspired the contour of the airfoil. First, the LaRC LFC program (Laminar Flow C

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Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2013-07-16 07:29:23
12Airfoil Technology  The historical evolution of airfoil sections, [removed]The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface.  Th

Airfoil Technology The historical evolution of airfoil sections, [removed]The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Th

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Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2014-08-11 17:14:13
13Revision 1.0 September, 1986 METHOD TO-8 METHOD FOR THE DETERMINATION OF PHENOL AND METHYLPHENOLS (CRESOLS) IN AMBIENT AIR USING HIGH PERFORMANCE LIQUID CHROMATOGRAPHY

Revision 1.0 September, 1986 METHOD TO-8 METHOD FOR THE DETERMINATION OF PHENOL AND METHYLPHENOLS (CRESOLS) IN AMBIENT AIR USING HIGH PERFORMANCE LIQUID CHROMATOGRAPHY

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Source URL: www.epa.gov

Language: English - Date: 2010-08-24 16:14:04
14Residence time of buoyant objects in drowning machines Gustavo Gioiaa, Pinaki Chakrabortyb,1, Stefan F. Garya,2, Carlo Zuñiga Zamalloaa, and Richard D. Keanea a Department of Mechanical Science and Engineering, Universi

Residence time of buoyant objects in drowning machines Gustavo Gioiaa, Pinaki Chakrabortyb,1, Stefan F. Garya,2, Carlo Zuñiga Zamalloaa, and Richard D. Keanea a Department of Mechanical Science and Engineering, Universi

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Source URL: www.river-management.org

Language: English - Date: 2012-10-20 08:47:53
15Revision 1.0 September, 1986 METHOD TO-8 METHOD FOR THE DETERMINATION OF PHENOL AND METHYLPHENOLS (CRESOLS) IN AMBIENT AIR USING HIGH PERFORMANCE LIQUID CHROMATOGRAPHY

Revision 1.0 September, 1986 METHOD TO-8 METHOD FOR THE DETERMINATION OF PHENOL AND METHYLPHENOLS (CRESOLS) IN AMBIENT AIR USING HIGH PERFORMANCE LIQUID CHROMATOGRAPHY

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Source URL: www.epa.gov

Language: English - Date: 2010-08-24 16:14:04
16High Velocity Flow in Chanells having Steep-Sided Channel Walls

High Velocity Flow in Chanells having Steep-Sided Channel Walls

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Source URL: digital.library.okstate.edu

Language: English - Date: 2009-01-09 17:00:16
17Microsoft Word - Chapter 5 appendix title sheet.doc

Microsoft Word - Chapter 5 appendix title sheet.doc

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Source URL: www.tdot.state.tn.us

Language: English - Date: 2011-06-02 11:47:55
18AIAA[removed]3rd AIAA Flow Control Conference[removed]June 2006, San Francisco, California  Drag Reduction of Natural Laminar Flow Airfoils with a

AIAA[removed]3rd AIAA Flow Control Conference[removed]June 2006, San Francisco, California Drag Reduction of Natural Laminar Flow Airfoils with a

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Source URL: sinhatech.com

Language: English - Date: 2006-06-20 16:03:06
19Journal of Hydraulic Research Vol. 43, No[removed]), pp. 234–244 © 2005 International Association of Hydraulic Engineering and Research

Journal of Hydraulic Research Vol. 43, No[removed]), pp. 234–244 © 2005 International Association of Hydraulic Engineering and Research

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Source URL: espace.library.uq.edu.au

Language: English
20SUBSONIC AIRFOIL DESIGN HISTORICAL BACKGROUND From its very beginning, the National Advisory Committee for Aeronautics (NACA) recognized the importance of airfoils as a cornerstone of aeronautical research and development. In

SUBSONIC AIRFOIL DESIGN HISTORICAL BACKGROUND From its very beginning, the National Advisory Committee for Aeronautics (NACA) recognized the importance of airfoils as a cornerstone of aeronautical research and development. In

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Source URL: www.airfoils.com

Language: English - Date: 2000-06-21 17:15:10