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INFLUENCE OF STATIC AEROELASTICITY ON OBLIQUE WINGED AIRCRAFT.WEISSHAAR TA.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 247-249; BIBL. 5 REF.Article

THEORETICAL STUDY OF LIFT-GENERATED VORTEX WAKES DESIGNED TO AVOID ROLLUP.ROSSOV VJ.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 478-484; BIBL. 24 REF.Article

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

A SENSITIVE ROLLING MOMENT BALANCE FOR USE IN SUPERSONIC BLOWDOWN TUNNELSSUNDARA MURTHY H.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 9; PP. 799-800; BIBL. 3 REF.Article

PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 17-21; BIBL. 13 REF.Article

WIND TUNNEL MEASUREMENTS OF ROLLING MOMENT IN A SWEPT-WING VORTEX WAKE.EL RAMLY Z; RAINBIRD WJ; EARL DG et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 962-967; BIBL. 15 REF.Article

A SENSITIVE TORQUE METER FOR WIND-TUNNEL APPLICATIONS.SNEDEKER RS.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 3; PP. 314-315; BIBL. 1 REF.Article

NONLINEAR ROLLING MOTION OF A CANARD-CONTROLLED MISSILE CONFIGURATION AT ANGLES OF ATTACK FROM 0 TO 30 DEGREES IN INCOMPRESSIBLE FLOWHARDY SR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-61; 10 P.; BIBL. 7 P.Conference Paper

EXPERIMENTAL STUDY OF THE EFFECT OF SPAN LOADING ON AIRCRAFT WAKES.CORSIGLIA VR; ROSSOW VJ; CIFFONE DL et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 968-973; BIBL. 21 REF.Article

THEORETICAL PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 111; PP. 1-8; BIBL. 11 REF.Conference Paper

EFFECT OF THERMALLY EXPANDING SURFACES ON AERODYNAMIC ROLL TORQUES FOR CONESMCDEVITT JB.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 505-510; BIBL. 8 REF.Serial Issue

FINITE CHORD EFFECTS ON VORTEX INDUCED WING LOADS = EFFETS D'UNE CORDE FINIE SUR LES CHARGES-D'AILE INDUITES PAR LES TOURBILLONSFILOTAS LT.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 6; PP. 888-890; BIBL. 4 REF.Serial Issue

STUDY OF LOW-ASPECT RATIO SWEPT AND OBLIQUE WINGS.HOPKINS EJ; LEVIN AD.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 8; PP. 648-652; BIBL. 12 REF.Article

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