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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

ON NUMERICAL METHODS OF SUBSONIC LIFTING SURFACE THEORYANDO S; ICHIKAWA A; LEE DH et al.1982; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 24/1982-02-17/TEL-AVIV, HAIFA; ISR; HAIFA: IMPR. AYALON OFFSET; DA. 1982; PP. 87-99; BIBL. 20 REF.Conference Paper

AN INVISCID THEORY FOR SLIDING FLEXIBLE SHEETSTUCK EO.1982; J. AUST. MATH. SOC., SER. B, APPL. MATH.; ISSN 0334-2700; AUS; DA. 1982; VOL. 23; NO 4; PP. 403-415; BIBL. 7 REF.Article

A THEORETICAL TREATMENT OF LIFTING SURFACE THEORY OF AN ELLIPTIC WINGKIDA T.1980; Z. ENGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 12; PP. 645-651; ABS. GER/RUS; BIBL. 13 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

HYDRODYNAMIC CHARACTERISTICS OF A RING WING OF ELLIPTIC CROSS-SECTIONKHOLODILIN AN.1978; Z. ANGEW. MATH. MECH.; DDR; DA. 1978; VOL. 58; NO 7; PP. 280-282; BIBL. 2 REF.Article

LIFTING LINE THEORY FOR TRANSONIC FLOWCOOK LP; COLE JD.1978; S.I.A.M. J. APPL. MATH.; USA; DA. 1978; VOL. 35; NO 2; PP. 209-228; BIBL. 7 REF.Article

LIFTING SURFACE THEORY FOR THRUST-AUGMENTING EJECTORSBEVILAQUA PM.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 5; PP. 475-481; BIBL. 9 REF.Article

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

II. TRANSONIC COMPRESSOR.OKUROUNMU O; MCCUNE JE.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1372-1380; BIBL. 13 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

USE OF SIMPLIFIED FLOW SEPRATION CRITERIA FOR SLOTTED FLAP PRELIMINARY DESIGNWENTZ WH JR.1977; S.A.E. TRANS.; USA; DA. 1977 PUBL. 1978; VOL. 86; SECTION 3; PP. 2027-2035; BIBL. 8 REF.Article

LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 551; PP. 1-10; BIBL. 11 REF.Conference Paper

VISCOUS THIN AIRFOIL THEORY AND THE KUTTA CONDITIONYATES JE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-152; 7 P.; BIBL. 17 REF.Conference Paper

A THEORETICAL AND EXPERIMENTAL STUDY ON THE PLANFORM OF SUPERVENTILATED WINGS.TSEN LF; GUILBAUD M.1974; J. SHIP RES.; U.S.A.; DA. 1974; VOL. 18; NO 3; PP. 169-184; BIBL. 26 REF.Article

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

LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 7; PP. 519-524; BIBL. 11 REF.Article

TO THE PROBLEM OF STARTING AND AIRFOIL-SHAPE OPTIMIZATION OF THE SUPERSONIC COMPRESSOR CASCADECELIKOVSKY K; SAFARIK P.1978; ACTA TECH. C.S.A.V.; CSK; DA. 1978; VOL. 23; NO 6; PP. 732-754; BIBL. 18 REF.Article

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

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