Supercritical airfoil

Results: 23



#Item
1MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive and

MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive and

Add to Reading List

Source URL: www.fzt.haw-hamburg.de

Language: English - Date: 2005-10-26 05:29:51
2TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,

TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,

Add to Reading List

Source URL: www.logbookmag.com

Language: English - Date: 2012-02-24 02:11:55
3CALIFORNIA STATE SCIENCE FAIR 2014 PROJECT SUMMARY Name(s)  Reese A. Swanson

CALIFORNIA STATE SCIENCE FAIR 2014 PROJECT SUMMARY Name(s) Reese A. Swanson

Add to Reading List

Source URL: www.usc.edu

Language: English - Date: 2014-04-25 17:08:56
4National Aeronautics and Space Administration  NASA AERONAUTICS RESEARCH ONBOARD D E C A D E S O F C O N T R I B U T I O N S T O G E N E R A L AV I AT I O N 1

National Aeronautics and Space Administration NASA AERONAUTICS RESEARCH ONBOARD D E C A D E S O F C O N T R I B U T I O N S T O G E N E R A L AV I AT I O N 1

Add to Reading List

Source URL: www.nasa.gov

Language: English - Date: 2013-04-30 20:24:24
5[removed]:57 AM  NASA - Aviation Pioneer Richard T. Whitcomb , Log In To MyNASA

[removed]:57 AM NASA - Aviation Pioneer Richard T. Whitcomb , Log In To MyNASA

Add to Reading List

Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2014-08-21 11:54:54
6This 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

Add to Reading List

Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2013-07-16 07:29:23
7NATIONAL AERONAUT ICS AND SPACE ADM INISTRATION LANGLEY RESEARCH CENTER • HM1PTON, VI RG I N1,iI, 23365 THOMAS C. KELLY High -Speed Aircraft Division Thomas C. Kelly is group l eader in th~ 8-foot Tunnels Branch

NATIONAL AERONAUT ICS AND SPACE ADM INISTRATION LANGLEY RESEARCH CENTER • HM1PTON, VI RG I N1,iI, 23365 THOMAS C. KELLY High -Speed Aircraft Division Thomas C. Kelly is group l eader in th~ 8-foot Tunnels Branch

Add to Reading List

Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2014-04-30 14:21:32
8Airfoil 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

Add to Reading List

Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2014-08-11 17:14:13
9CALIFORNIA STATE SCIENCE FAIR 2014 PROJECT SUMMARY Name(s)  Reese A. Swanson

CALIFORNIA STATE SCIENCE FAIR 2014 PROJECT SUMMARY Name(s) Reese A. Swanson

Add to Reading List

Source URL: www.usc.edu

Language: English - Date: 2014-04-25 17:08:56
10~.  NewsRelease National Aeronautics and Space Administration

~. NewsRelease National Aeronautics and Space Administration

Add to Reading List

Source URL: crgis.ndc.nasa.gov

Language: English - Date: 2013-07-30 13:56:38