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kw.\*:("CONFIGURATION CANARD")

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TRIMMED DRAG AND MAXIMUM FLIGHT EFFICIENCY OF AFT TAIL AND CANARD CONFIGURATIONS.GOLDSTEIN SE; COMBS CP.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 69; PP. 1-12; BIBL. 5 REF.Conference Paper

LOAD DISTRIBUTION ON A CLOSE-COUPLED WING CANARD AT TRANSONIC SPEEDS.GLOSS BB; WASHBURN KE.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 4; PP. 234-239; BIBL. 15 REF.Article

INTERACTION AERODYNAMIQUE ENTRE UN CANARD PROCHE ET UNE AILE EN FLECHE EN ECOULEMENT TRANSSONIQUEBROCARD Y; SCHMITT V.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 23 P.; ABS. ENG; BIBL. 15 REF.Conference Paper

A MODEL FOR THE EVALUATION OF INDUCED ROLLING MOMENTS AND SIDE FORCES IN SLENDER CRUCIFORM CANARD CONFIGURATIONS AT SMALL ANGLES OF INCIDENCE.GUR I; SHINAR J; ROM J et al.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 74-85; BIBL. 18 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper

TRANSONIC FLOW CALCULATIONS OVER TWO-DIMENSIONAL CANARD-WING SYSTEMSVIJAYA SHANKAR; MALMUTH ND; COLE JD et al.1981; J. AICR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 2; PP. 108-114; BIBL. 12 REF.Article

A LARGE-SCALE LOW-SPEED TUNNEL TEST OF A CANARD CONFIGURATION WITH SPANWISE BLOWING.JENKINS MWM; MEYER RT.1975; IN: AM. INST. AERONAUT. ASTRONAUT AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 994; PP. 1-9; BIBL. 2 REF.Conference Paper

CANARD-WING VORTEX EFFECTS IN SUBSONIC FLOWDE SILVA BME; MEDAN RT.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 1; PP. 5-6; BIBL. 6 REF.Article

STATIC AEROELASTIC EFFECTS ON THE AERODYNAMICS OF THE SAAB 37 VIGGEN AIRCRAFT, A COMPARISON BETWEEN CALCULATIONS, WINDTUNNEL TESTS AND FLIGHT TESTS.KLOOS J; ELMELAND L.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 438-446; BIBL. 3 REF.Conference Paper

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