Etude de faisabilité d'essais en soufflerie multisites menés en coopération, en vue de la validation des calculs de l'aérodynamique numérique - CFD PDF
By:North Atlantic Treaty Organization. Research and Technology Organization. Applied Vehicle Technology Panel. Working Group 011
Published on 1999 by
Between 1997 and 1999, a Working Group on the feasibility of collaborative, multi-facility windtunnel testing for the validation of Computational Fluid Dynamics Codes (CFD) has established the following results: Wintunnel tests are the main source of CFD validation but all have specific bias errors. Testing of the same model in several facilities can better establish the level of uncertainty in windtunnel tests and hence help assess possible differences between CFD and windtunnel tests. The Working Group, after an initial inquiry, established the need for CFD validation for fighter aircraft, transport type aircraft, missiles and helicopters. Effort and cost can be controlled efficiently and would permit the improvement of CFD Codes for considerable cost saving in future developments.
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