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