Forum: Main CFD Forum
January 19, 2011, 22:23
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Replies: 4
Views: 4,291
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Forum: Main CFD Forum
January 19, 2011, 21:23
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Replies: 4
Views: 4,291
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Forum: Main CFD Forum
January 17, 2011, 09:43
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Replies: 4
Views: 4,291
Highest LD ratio designs
can someone give the technical name or coordinate files of airfoils having highest LD ratio; above 50
also tell me how to generate a sears hack body's coordinate file
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Forum: Main CFD Forum
February 21, 2010, 21:57
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Replies: 2
Views: 1,361
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Forum: Main CFD Forum
February 21, 2010, 12:47
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Replies: 2
Views: 1,361
Zero Pressure Drag Design
I had invented a new aerodynamic concept to reduce drag. The CFD analysis shows Horizontal velocity vectors at Trailing edge. I think this implies zero pressure drag, since all the kinetic energy...
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Forum: Main CFD Forum
February 7, 2010, 03:36
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Replies: 25
Views: 7,368
Actually both Tangents at trailing edge is...
Actually both Tangents at trailing edge is horizontal but cusp is more general term cycloid is only a member of that group. can you suggest a link of the article "A boundary integral equations...
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Forum: Main CFD Forum
February 6, 2010, 19:49
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 19:29
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 13:03
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 09:27
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 08:00
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 07:25
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 6, 2010, 03:19
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Replies: 25
Views: 7,368
The lift in airfoil is generated by pressure...
The lift in airfoil is generated by pressure difference; the lower pressure in upper side of wing is due to higher velocity of air. I am only tryin to make vertical component of velocity zero at...
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Forum: Main CFD Forum
February 6, 2010, 01:15
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Replies: 25
Views: 7,368
even if front is blunt the rest of the body...
even if front is blunt the rest of the body profile is cycloid or combination of cycloid. But I never heard cycloid is used as thickness function of any airfoil.
Also worth mentioning is that you...
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Forum: Main CFD Forum
February 5, 2010, 23:13
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 5, 2010, 22:50
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 5, 2010, 22:47
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 5, 2010, 14:28
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Replies: 25
Views: 7,368
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Forum: Main CFD Forum
February 5, 2010, 13:32
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Replies: 25
Views: 7,368
Secret Aerodynamics of B2 Stealth
I had invented a new aerodynamic concept to reduce drag. My friends and colleagues say that my concept has striking similarity to B2 Stealth Bomber (elevation) design. I think my concept is novel and...
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Forum: Main CFD Forum
February 1, 2010, 09:23
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Replies: 6
Views: 1,772
i used K-epsilon model and
for comparison ...
i used K-epsilon model and
for comparison NACA 4412 airfoil is used.
The freestream velocity is 50 m/s
Pressure = 101,325 Pa
Density = 1.2250 kg/m3
Temperature = 288.16 K
Kinematic...
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Forum: Main CFD Forum
February 1, 2010, 08:39
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Replies: 6
Views: 1,772
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Forum: Main CFD Forum
February 1, 2010, 02:31
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Replies: 6
Views: 1,772
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Forum: Main CFD Forum
January 31, 2010, 22:17
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Replies: 6
Views: 1,772
Highly aerodynamic design
I have invented a new aerodynamic shape with low drag. I am looking for your esteemed feedback on the concept. Technical details are given in site...
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Forum: Main CFD Forum
January 17, 2010, 02:35
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Replies: 0
Views: 1,505
Exhaust less Nuclear Space Propulsion
I have invented a new space propulsion device can you help me in improving or implementing the concept. The details are given in site : http://sites.google.com/site/exhaustlessnuclearpropulsion/
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Forum: Main CFD Forum
January 15, 2010, 08:28
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Replies: 24
Views: 6,406
built in modeler of AVL fire may have limited...
built in modeler of AVL fire may have limited features as in other CFD programs. but it supports step or iges files. Unlike CFX, AVL Fire is specifically designed by AVL for IC engines, major...
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