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VERSUCH
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TEXUS 52, TEXUS 53 : Schlussberichte ; Experimentelle Nutzlast
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
Prediction of the flow around the X-31 aircraft using three different CFD methods