kw.\*:("LIFTING SURFACE THEORY")
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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
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
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
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
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
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
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
OSCILLATING AIRFOILS. II: NEWTONIAN FLOW THEORY AND APPLICATION TO POWERLAW BODIES IN HYPERSONIC FLOWBARRON RM; MANDL P.1978; A.I.A.A. J.; USA; DA. 1978; VOL. 16; NO 11; PP. 1132-1138; BIBL. 10 REF.Article
A FINITE STATE AERODYNAMIC MODEL FOR A LIFTING SURFACE IN INCOMPRESSIBLE FLOWMIYAZAWA Y; WASHIZU K.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 163-171; BIBL. 16 REF.Article
RELIABLE LIFTING SURFACE SOLUTIONS FOR UNSTEADY FLOWJORDAN PF.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 9; PP. 626-633; BIBL. 12 REF.Article
SOME EXPERIMENTAL RESULTS CONNECTED WITH THE TRANSONIC INSTABILITIES ON AN AIRFOILVLCEK V.1978; STROJN. CAS.; CSK; DA. 1978; VOL. 29; NO 3; PP. 342-354; ABS. SLO; BIBL. 4 REF.Article
AERODYNAMICS OF WINGS IN SUBSONIC SHEAR FLOWBARSONY NAGY A; HANIN M.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 4; PP. 451-456; BIBL. 11 REF.Article
EFFECT OF FORWARD ACCELERATION ON AERODYNAMIC CHARACTERISTICS OF WINGSANDO S; ICHIKAWA A.1979; A.I.A.A. J., NEW YORK; USA; DA. 1979; VOL. 17; NO 6; PP. 653-655; BIBL. 7 REF.Article
MISE AU POINT D'UNE APPROXIMATION INITIALE POUR LA RESOLUTION DE L'EQUATION INTEGRALE RELATIVE A UNE SURFACE PORTANTEMEL'NIKOVA OF; POLYAKHOV NN.1979; VEST. LENINGRAD. UNIV.; SUN; DA. 1979; NO 1; PP. 104-110; BIBL. 6 REF.Article
AN ALTERNATIVE TREATMENT OF LIFTING-LINE THEORY AS A PERTURBATION PROBLEMKIDA T; MIYAI Y.1978; Z. ANGEW. MATH. PHYS.; CHE; DA. 1978; VOL. 29; NO 4; PP. 591-607; ABS. GER; BIBL. 3 REF.Article