HIGH-FREQUENCY SUBSONIC FLOW PAST A PULSATING THIN AIRFOIL.PLOTKIN A.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 4; PP. 405-407; BIBL. 8 REF.Article

SECTION DESIGN FOR HYDROFOIL WINGS WITH FLAPSSHEN YT; EPPLER R.1979; J. HYDRONAUT.; USA; DA. 1979; VOL. 13; NO 2; PP. 39-45; BIBL. 14 REF.Article

TURBULENT AIRFOILS FOR GENERAL AVIATION.EPPLER R.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 93-99; BIBL. 21 REF.Article

A POTENTIAL FLOW DESIGN METHOD FOR MULTICOMPONENT AIRFOIL SECTIONS.KENNEDY JL; MARSDEN DJ.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 1; PP. 47-52; BIBL. 8 REF.Article

SMALL PERTURBATION EXPANSIONS IN UNSTEADY AEROFOIL THEORY.GRAHAM JMR; KULLAR I.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 83; NO 2; PP. 209-224; BIBL. 22 REF.Article

DECAY AND MODIFICATION OF TRAILING VORTEX.TANAKA S; KAIBARA M; TANAKA A et al.1978; BULL. J.S.M.E.; JAP.; DA. 1978; VOL. 21; NO 151; PP. 98-103; BIBL. 4 REF.Article

THEORIE ASYMPTOTIQUE D'UNE AILE SE MOUVANT A DE PETITES DISTANCES D'UNE PAROI RIGIDEROZHDESTVENSKIJ KV.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 115-124; BIBL. 5 REF.Article

ON-LINE COMPUTER DETERMINATION OF THE UNSTEADY LIFT CHARACTERISTICS OF HYDROFOILS BY A MULTI-FREQUENCY TECHNIQUE.FLOWER JO; FORGE SC; KNOTT G et al.1976; INTERNATION. SHIPBUILDG PROGR.; NETHERL.; DA. 1976; VOL. 23; NO 265; PP. 313-316; BIBL. 6 REF.Article

ON THE CALCULATION OF THE INCOMPRESSIBLE FLOW PAST AN AEROFOIL WITH A JET FLAP.O'MAHONEY R; SMITH FT.1978; AERONAUT. QUART.; G.B.; DA. 1978; VOL. 29; NO 1; PP. 44-59; BIBL. 1 P.Article

EXPERIMENTAL VERIFICATION OF AN ANNULAR AEROFOIL THEORY.PIVKO S.1977; ACAD. SERBE SCI. ARTS, BULL., CL. SCI. TECH.; YOUGOSL.; DA. 1977; VOL. 57; NO 11; PP. 65-70; BIBL. 3 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

AN EXPERIMENT ON THE LIFT OF AN ACCELERATED AIRFOIL.MINKKINEN GT; WILSON TA; BEAVERS GS et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 5; PP. 687-689; BIBL. 3 REF.Article

EXPLICIT AND IMPLICIT CORRECTED VISCOSITY SCHEMES FOR THE COMPUTATION OF STEADY TRANSONIC FLOWSESSERS JA.1982; CONFERENCE ON NUMERICAL METHODS IN FLUID MECHANICS. 4/1981/PARIS; DEU; BRAUNSCHWEIG; WIESBADEN: F. VIEWEG; DA. 1982; PP. 106-116; BIBL. 7 REF.Conference Paper

AN ASYMPTOTIC EXPRESSION OF LIFT SLOPE OF ELLIPTIC WING WITH HIGH ASPECT RATIOKIDA T.1982; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1982; VOL. 62; NO 9; PP. 491-493; BIBL. 10 REF.Article

EVALUATION STUDY OF A THREE-SPEED HYDROFOIL WITH WETTED UPPER SIDEROWE A.1979; J. SHIP RES.; USA; DA. 1979; VOL. 23; NO 1; PP. 55-65; BIBL. 24 REF.Article

VARIATIONAL PRINCIPLES FOR THE TRANSONIC AIRFOIL PROBLEM.CAREY GF.1978; COMPUTER METHODS APPL. MECH. ENGNG; NETHERL.; DA. 1978; VOL. 13; NO 2; PP. 129-140; BIBL. 11 REF.Article

THE DESIGN OF LIFTING SUPERCRITICAL AIRFOILS USING A NUMERICAL OPTIMIZATION METHOD.EGGLESTON B; JONES DJ.1977; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1977; VOL. 23; NO 3; PP. 172-181; BIBL. 12 REF.Article

WIND-TUNNEL WALL INTERFERENCE EFFECTS ON A SUPERCRITICAL AIRFOIL AT TRANSONIC SPEEDS.BLACKWELL JA JR; POUNDS GA.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 929-935; BIBL. 6 REF.Article

LIFTING WINGS AND BODIES AT SUPERSONIC AND HYPERSONIC SPEEDS. EUROMECH 74; CAMBRIDGE; 1976.sd; S.L.; DA. S.D.; PP. (11P.)Conference Paper

DAS FERNFELD EINES TRAGFLUEGELS = LE CHAMP LOINTAIN D'UNE AILE PORTANTEOSWATITSCH K.1982; ING.-ARCH.; ISSN 0020-1154; DEU; DA. 1982; VOL. 52; NO 5; PP. 287-295; ABS. ENG; BIBL. 5 REF.Article

FOILBORNE HYDRODYNAMIC PERFORMANCE OF JETFOILNOREEN AE; GILL PR; FEIFEL WM et al.1980; J. HYDRONAUT.; USA; DA. 1980; VOL. 14; NO 2; PP. 56-62; BIBL. 7 REF.Article

DEFORMATION CURVE OF ROTARY AIRFOIL BLADES.NENADOVICH M.1977; ACAD. SERBE SCI. ARTS, BULL., CL. SCI. TECH.; YOUGOSL.; DA. 1977; NO 12; PP. 57-61; BIBL. 2 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

A SUMMARY REPORT OF MAJOR STUDIES UNDER THE PROGRAMME "HIGH SPEED HYDROFOIL STRUTS AND FOILS".WERMTER R; SHEN YT.1977; HOVERG CRAFT HYDROFOIL; G.B.; DA. 1977; VOL. 16; NO 7-8; PP. 44-51; BIBL. 40 REF.Article

ANALYSIS OF UNSTEADY VISCOUS FLOW PAST AN AIRFOIL. I. THEORETICAL DEVELOPMENT.KINNEY RB; CIELAK ZM.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 1712-1717; BIBL. 18 REF.Article