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VERSUCH
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An integrated computational/experimental approach to X-31 stability & control estimation
Experimental aerodynamic assessment and evaluation of an agile highly swept aircraft configuration
Experimental aerodynamic assessment and evaluation of an agile highly swept aircraft configuration
Prediction of the flow around the X-31 aircraft using three different CFD methods
TEXUS 52, TEXUS 53 : Schlussberichte ; Experimentelle Nutzlast