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EFFECTS OF WING BEND ON THE AERODYNAMIC CHARACTERISTICS OF A LOW ASPECT RATIO OBLIQUE WING.HOPKINS EJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 995; PP. 1-5; BIBL. 10 REF.Conference Paper

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

COMPRESSIBLE FLOW CALCULATIONS BY A VARIATIONAL METHOD USING NATURAL BOUNDARY CONDITIONS.RASMUSSEN H.1976; J. INST. MATH. APPL., LONDON; G.B.; DA. 1976; VOL. 17; NO 7; PP. 111-118; BIBL. 6 REF.Article

CALCULATION OF A TRANSONIC LIFTING LINE THEORYSMALL RD.1981; ISR. J. TECHNOL.; ISSN 0021-2202; ISR; DA. 1981; VOL. 19; NO 1-2; PP. 26-33; BIBL. 7 REF.Conference Paper

PADE APPROXIMATION APPLIED TO FLOW PAST THIN AIRFOILSVENKATARANGAN SN; NARENDRAN G.1980; J. MATH. & PHYS. SCI.; ISSN 0047-2557; IND; DA. 1980; VOL. 14; NO 5; PP. 485-489; BIBL. 2 REF.Article

PRESSURE DISTRIBUTION AND CAVITY MODEL ON A PARTIALLY CAVITATING HYDROFOIL OF FINITE SPAN.UKON Y; TAMIYA S; KATO H et al.sdIN: INT. TOWING TANK CONF. 14. PROC., OTTAWA; 1975; OTTAWA; NATL. RES. COUNC. CAN.; DA. S.D.; VOL. 2; PP. 266-275; BIBL. 3 REF.Conference Paper

A CORRECTION TO "LIFTING-LINE THEORY AS A SINGULAR PERTURBATION PROBLEM"KERNEY KP.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1683-1684; BIBL. 6 REF.Serial Issue

ETUDE NUMERIQUE ET ASYMPTOTIQUE DE NAPPES TOURBILLONNAIRES ENROULEESHUBERSON SERGE.1979; ; FRA; DA. 1979; 63-9 P.: ILL.; 30 CM; BIBL. 20 REF.; TH. 3E CYCLE: MATH., MEC./PARIS 6/1979Thesis

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