kw.\*:("BORD ATTAQUE AIGU")
Results 1 to 8 of 8
Selection :
TRAGENDE SCHNABELPROFILE IN STOSSFREIER SCHALLANSTROEMUNG. = PROFILS PORTANTS A BORDS D'ATTAQUE AIGUS DANS UN ECOULEMENT INCIDENT TRANSSONIQUE SANS CHOCSOBIECZKY H.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 6; PP. 819-830; ABS. ANGL.; BIBL. 4 REF.Article
UNSTEADY AERODYNAMICS OF SLENDER DELTA WINGS AT LARGE ANGLES OF ATTACK.ERICSSON LE; REDING JP.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 721-729; BIBL. 41 REF.Article
FLOW REGIMES OVER DELTA WINGS AT SUPERSONIC AND HYPERSONIC SPEEDS.SQUIRE LC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 1; PP. 1-14; BIBL. 16 REF.Article
HYPERSONIC INCIPIENT SEPARATION ON DELTA WING WITH TRAILING-EDGE FLAP. = DECOLLEMENT HYPERSONIQUE NAISSANT SUR UNE AILE DELTA A VOLET DE BORD DE FUITEDHANVADA RAO.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1386-1388; BIBL. 9 REF.Article
TURBULENT DRAG COEFFICIENTS OF SHARP-EDGED OBJECTS.GRAF WH; MANSOUR FF.1975; J. RECH. HYDRAUL.; PAYS-BAS; DA. 1975; VOL. 13; NO 2; PP. 127-147; BIBL. 14 REF.Article
AERODYNAMIC HEATING IN GAPS IN THE PRESENCE OF PERTURBANCES AND SHOCK WAVE IMPINGEMENT.HUNG FT; STOTTOLINE CA.1975; IN: AM. INST. AERONAUT. ASTRONAUT. 10TH THERMOPHYS. CONF.; DENVER, COLO.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 655; PP. 1-7; BIBL. 15 REF.Conference Paper
LIFT AUGMENTATION ON A MODERATELY SWEPT WING BY SPANWISE BLOWING.CLARKE KP.1976; AERONAUT. J.; G.B.; DA. 1976; VOL. 80; NO 790; PP. 447-451; BIBL. 9 REF.Article
ON THE FLUID MECHANICS OF THE INHERENT RESTRICTOR.HAGERUP HJ.1974; J. FLUIDS ENGNG; U.S.A.; DA. 1974; VOL. 96; NO 4; PP. 341-347; BIBL. 5 REF.Article