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SWING WING. MODIFICATIONS IN VARIABLE GEOMETRY CONFIGURATION CONCEPTS = L'AILE PIVOTANTE. MODIFICATIONS DANS LES CONCEPTS DE CONFIGURATIONS A GEOMETRIE VARIABLEBIRD WJ.1973; AIRCR. ENGNG; G.B.; DA. 1973; VOL. 45; NO 3; PP. 12-16 (4 P.)Serial Issue

METHODE APPROCHEE POUR LE CALCUL DES CARACTERISTIQUES AERODYNAMIQUES DES AILES SEMI-ANNULAIRES A FLECHE CONSTANTE LE LONG DE L'ENVERGUREPASTUKHOV AI; KUDRYAVTSEV GS.1975; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1975; VOL. 18; NO 2; PP. 106-111; BIBL. 1 REF.Article

RECENT CONTRIBUTIONS TO THE SOLUTION OF NONLINEAR AERODYNAMIC INTERFERENCE PROBLEMS.HUMMEL D.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 229-243; BIBL. 1 P. 1/2Conference Paper

SLENDER DELTA WING WITH CONICAL CAMBER.BERA RK.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 245-247; BIBL. 7 REF.Article

AN ALTERNATIVE TREATMENT OF BOUNDARY CONDITIONS FOR THE FLOW OVER THICK WINGS.NIXON D.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 2; PP. 90-96; BIBL. 15 REF.Article

ETUDE EXPERIMENTALE D'UNE AILE EN ARC D'UNE ENVERGURE FINIE ET PRODUISANT UNE CAVITATIONMAL'TSEV LI; SADOVSKAYA NA.1976; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1976; NO 1; PP. 81-84Article

AERODYNAMIQUE D'UNE AILE PORTANTE ANNULAIREPIVKO S.1977; SRPSKA AKAD. NAUKA UMETN., POSEB. IZD., TEKH. NAUKA; YUGOSL.; DA. 1977; NO 12; PP. 1-100; ABS. ANGL.; BIBL. 1 P. 1/2Serial Issue

ECOULEMENT SUR LES SURFACES INFERIEURES DES AILES EN V EN REGIMES DESADAPTES POUR DES NOMBRES DE MACH, INFERIEURS A CELUI DU CALCULGUN'KO YU P; MAZHUL II.1977; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH NAUK; S.S.S.R.; DA. 1977; NO 3 PART. 1; PP. 8-12; BIBL. 8 REF.Article

A NOTE ON "LIFTING THREE-DIMENSIONAL WINGS IN TRANSONIC FLOW" BY M. S. CRAMERCRAMER MS.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 109; PP. 257-258; BIBL. 3 REF.Article

LOAD DISTRIBUTIONS ON SLENDER DELTA WINGS HAVING VORTEX FLOW.KUHLMAN J.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 699-702; BIBL. 8 REF.Article

THE FLOW OVER A "HIGH" ASPECT RATIO GOTHIC WING AT SUPERSONIC SPEEDS.YEGNA NARAYAN K.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 3; PP. 189-201; BIBL. 10 REF.Article

THE ROLE OF THE NAE 5-FOOT X 5-FOOT WIND TUNNEL IN THE DEVELOPMENT OF MODERN AIRFOIL SECTIONS.OHMAN LH.1975; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1975; NO 3; PP. 1-39; BIBL. 2 P. 1/2Article

QUELQUES PROBLEMES DE LA METHODE D'ETUDE DE LA CHARGE REPARTIE SUR DES AILES VIBRANTESVOLOGODSKIJ VB; IVANOV VV; LAGUTIN VI et al.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 5; PP. 178-181; BIBL. 4 REF.Article

THEORIE DE L'AILE DE FAIBLE ALLONGEMENT DANS UN ECOULEMENT HYPERSONIQUEGOLUBKIN VN.1980; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1980; NO 4; PP. 112-117; BIBL. 11 REF.Article

SPANWISE CAMBERED DELTA WING WITH LEADING-EDGE SEPARATION.FERNANDEZ J; HOLLA VS.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 3; PP. 276-282; BIBL. 14 REF.Article

LIFT AND MOMENT FLUCTUATIONS OF A CAMBERED ACROFOIL UNDER NONCONVECTING STREAMWISE GUST.RAO SSP; MUKHOPADHYAY V; RAO JS et al.1977; AERONAUT. J.; G.B.; DA. 1977; VOL. 81; NO 794; PP. 83-87; BIBL. 8 REF.Article

EMBEDDED FLOW CHARACTERISTICS OF SHARP-EDGED RECTANGULAR WINGSLARSON ES.1983; JOURNAL OF AIRCRAFT; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 3; PP. 193-194; BIBL. 5 REF.Article

A THIN AIRFOIL SPLINE PANEL METHODNAPOLITANO M; VACCA G.1981; MECCANICA; ISSN 0025-6455; ITA; DA. 1981; VOL. 16; NO 1; PP. 30-32; ABS. ITA; BIBL. 9 REF.Article

AEROELASTIC STABILITY AND CONTROL OF AN OBLIQUE WING.JONES RT; NISBET JW.1976; AERONAUT. J.; G.B.; DA. 1976; VOL. 80; NO 788; PP. 365-369; BIBL. 3 REF.Article

AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING WITH A TIP CLEARANCE IN A CHANNEL.SUGIYAMA Y.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 4; PP. 541-547; BIBL. 8 REF.Article

DESIGN STUDY OF STRUCTURAL CONCEPTS FOR AN ARROW-WING SUPERSONIC-CRUISE AIRCRAFT.SAKATA IF; DAVIS GW; ROBINSON JC et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1037; PP. 1-12; BIBL. 3 REF.Conference Paper

ZUR THEORIE DER VERAENDERLICHEN TRAGFLUEGELPFEILUNG. = THEORIE DE L'AILE A GEOMETRIE VARIABLEKORDIK EJT.1974; OESTERR. INGR-Z.; OESTERR.; DA. 1974; VOL. 17; NO 12; PP. 418-427; BIBL. 14 REF.Article

CALCUL DU FLUAGE D'UNE AILE A PAROIS MINCES SUR LA BASE DE L'ANALOGIE PLANESHATAEV VG.1972; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1972; NO 4; PP. 67-72; BIBL. 7 REF.Serial Issue

ANWENDUNG UND VERGLEICH MODALER PERTURBATIONSMETHODEN UND MODALER KORREKTURVERFAHREN AM BEISPIEL EINES PFEILFLUEGELS MIT ZWEI PYLONAUSSENLASTEN. = MODIFICATIONS DE STRUCTURE D'UNE MAQUETTE D'AILE FLECHE A DEUX CHARGES EXTERIEURES AU MOYEN DES METHODES DE PERTURBATIONS MODALES ET DE CORRECTIONS MODALESFREYMANN R.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 21; PP. 1-43; ABS. ANGL.; BIBL. 7 REF.Serial Issue

ETUDE EXPERIMENTALE DE LA RESISTANCE DES AILES AUX VITESSES SUPERSONIQUESBRODETSKIJ MD; KOSORYGIN VS; RAFAEHLYANTS AA et al.1977; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1977; NO 2; PP. 47-53; BIBL. 8 REF.Article

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