AUTOMATISIERTE MESSWERTERFASSUNG BEI STROEMUNGSMESSUNGEN IM WINDKANAL. = ENREGISTREMENT AUTOMATIQUE DES RESULTATS DE MESURES EN SOUFFLERIEBEGER G; GERLACH K; HAUKE W et al.1974; MASCHINENBAUTECHNIK; DTSCH.; DA. 1974; VOL. 23; NO 9; PP. 410-413; ABS. RUSSE ANGL.Article

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