Computation of 3-D transonic flows for wings and wing-body configurations

Chakrabartty, SK and Subramanian, NR (1988) Computation of 3-D transonic flows for wings and wing-body configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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The transonic full potential code using' body fitted coordinates with ADI/AF2 scheme is under development . The, code was evaluated for the test case of RAE WING A (Wing alone case) for three conditions, namely (1) Mach number =0 .8, and zero incidence, (2) Mach number =0 .8 ) incidence of 2 xB0;, and (3) Mach number =0 .9 and incidence 18 . Comparison with results of an available code is given . The present results show the same trend of pressure distribution as observed in experiments and' calculation for the wing-body case . The work on applying the present code to wing-- body case is in progress .13; Also, the time taken for a typical run has been considerably reduced to the order of 1 hour of CPU on NAL computer .

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Wing-body configuration;Transonic flow
Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
Depositing User: Users 60 not found.
Date Deposited: 08 Aug 2006
Last Modified: 24 May 2010 04:15

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