LIFTING-SURFACE THEORY FOR A SEMI-INFINITE WING IN OBLIQUE GUST.SING CHU; WIDNALL SE.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1672-1678; BIBL. 15 REF.Article

QUADRATURE FORMULAS FOR CHORDWISE INTEGRALS OF LIFTING SURFACE THEORIESANDO S; ICHIKAWA A.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 3; PP. 466-467; BIBL. 6 REF.Article

AIRFAIL WITH MINIMUM RELAXATION DRAGBUGGISCH H; ELLERMEIER W; WELLMANN J et al.1979; ARCH. MECH.; POL; DA. 1979; VOL. 31; NO 3; PP. 339-351; ABS. POL/RUS; BIBL. 9 REF.Article

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UNSTEADY LIFTING-SURFACE THEORY FOR SHIP SCREWS: DERIVATION AND NUMERICAL TREATMENT OF INTEGRAL EQUATION = THEORIE INSTATIONNAIRE DES SURFACES PORTANTES POUR HELICES MARINES: ETABLISSEMENT ET TRAITEMENT NUMERIQUE DE L'EQUATION INTEGRALEVAN GENT W.1975; J. SHIP RES.; U.S.A.; DA. 1975; VOL. 18; NO 4; PP. 243-253; BIBL. 18 REF.Article

COMMENTS ON JACOBS AND TSAKONAS: "PROPELLER LOADING-INDUCED VELOCITY FIELD BY MEANS OF UNSTEADY LIFTING SURFACE THEORY"GOODMAN TR.1982; J. SHIP RES.; ISSN 0022-4502; USA; DA. 1982; VOL. 26; NO 4; PP. 266-268Article

RELIABLE LIFTING SURFACE SOLUTIONS FOR UNSTEADY FLOWJORDAN PF.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-228; 10 P.; BIBL. 12 REF.Conference Paper

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A LIFTING SURFACE THEORY FOR THE SOUND GENERATED BY THE INTERACTION OF VELOCITY DISTURBANCES WITH A LEANED VANE STATORSCHULTEN JBHM.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 14 P.; BIBL. 15 REF.Conference Paper

ON LIFTING SURFACES IN UNSTEADY FLOWJORDAN PF.1980; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T193-T194; BIBL. 1 REF.Article

COMPUTER-AIDED DESIGN: AERODYNAMICSHAINES AB.1979; AERONAUT. J.; GBR; DA. 1979; VOL. 83; NO 819; PP. 81-91; BIBL. 29 REF.Article

MEASUREMENTS OF NOISE PRODUCED BY FLOW PAST LIFTING SURFACESKENDALL JM.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-239; 11 P.; BIBL. 12 REF.Conference Paper

A SIMPLIFIED METHOD OF INTEGRATING THE EQUATION OF THE LIFTING SURFACE AND ITS CONNECTION WITH A CERTAIN SYSTEM OF LIFTING LINESNOWAK M.1979; BULL. ACAD. POLON. SCI., SCI. TECH.; POL; DA. 1979; VOL. 27; NO 1; PP. 63-68; ABS. RUS; BIBL. 2 REF.Article

A VISUAL INVESTIGATION OF THE SEPARATION AND SUBSEQUENT TRANSITION NEAR THE LEADING EDGE OF AIRFOILSARENA AV.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 552; 10 P.; BIBL. 9 REF.Conference Paper

THREE-DIMENSIONAL POTENTIAL FLOW THROUGH A RECTILINEAR CASCADE OF BLADES.FALCAO AF DE O.1975; INGR-ARCH.; DTSCH.; DA. 1975; VOL. 44; NO 1; PP. 27-41; ABS. ALLEM.; BIBL. 12 REF.Article

SIMPLIFIED SOLUTION OF THE COMPRESSIBLE LIFTING SURFACE PROBLEMPURVIS JW; BURKHALTER JE.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 11 P.; BIBL. 26 REF.Conference Paper

THE EFFECT OF CHORDWISE FLEXIBILITY ON THE LIFT OF A RAPIDLY ACCELERATED AIRFOILKATZ J; WEIHS D.1979; AERONAUT. QUART.; GBR; DA. 1979; VOL. 30; NO 1; PP. 360-370; BIBL. 12 REF.Article

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LIFTING SURFACE THEORY OF AXIAL COMPRESSOR BLADE ROWS. I. SUBSONIC COMPRESSOR.OKUROUNMU O; MCCUNE JE.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1363-1372; BIBL. 11 REF.Article

OSCILLATORY SUPERSONIC KERNEL FUNCTION METHOD FOR INTERFERING SURFACES.CUNNINGHAM AM JR.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 11; PP. 664-670; BIBL. 11 REF.Article

LINEARIZED THREE-DIMENSIONAL POTENTIAL FLOW THROUGH A RECTILINEAR CASCADES OF BLADES.DE O FALCAO AF.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 16 REF.Conference Paper

EFFETTO DELLO SPESSORE NEL CALCOLO DI FORZE AERODINAMICHE GENERALIZZATE SU UN' ALA OSCILLANTE. = EFFET DE L'EPAISSEUR SUR LE CALCUL DES FORCES AERODYNAMIQUES GENERALISEES SUR UNE AILE OSCILLANTESANTINI P; CARLINI O; OGNIBENE L et al.sdIN: SATELL. METEOROL. RISORSE TERREST. TECNOL. SPEC. COLLAB. INT. ATTI XIV CONV. INT. SPAZIO; ROMA; 1974; ROMA; RASSEGNA INT. ELETTRON. NUCL. AEROSP.; DA. S.D.; PP. 153-159; ABS. ANGL.; BIBL. 3 REF.Conference Paper