kw.\*:("AILE PORTANTE")
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AUSLEGUNG VON UNGEPFEILTEN TRAGFLUEGELN GROSSEN SEITENVERHAELTNISSES MIT WOELBKLAPPEN FUER ZWEI ENTWURFSPUNKTE. = PROJET D'AILES PORTEUSES AYANT UN RAPPORT DE COTES IMPORTANT, MUNIES DE CLAPETS POUR 2 CONDITIONS DE VOLREDEKER G.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 34; PP. 1-36; ABS. ANGL.; BIBL. 8 REF.Article
A CONCEPTUAL STUDY FOR A NEW WINGED SURFACE EFFECT VEHICLE SYSTEM = UNE ETUDE CONCEPTUELLE DE NOUVEAU SYSTEME DE VEHICULE A EFFET DE SURFACE MUNI D'AILESMCMASTERS JH; GREER RR.1974; NAV. ENGRS J.; U.S.A.; DA. 1974; VOL. 86; NO 2; PP. 41-51; BIBL. 10 REF.Article
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
ZUM AUFTRIEBSPROBLEM VON TRAGFLUEGELN MIT WOELBUNG UND VERWINDUNG BEI UEBERSCHALLSTROEMUNG. = PROBLEME DE PORTANCE DES AILES PORTANTES AVEC CAMBRURE ET GAUCHISSEMENT DANS DES ECOULEMENTS SUPERSONIQUESDAS A.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 10; PP. 1-60; ABS. ANGL.; BIBL. 3 P.Article
DOUBLET LATTICE-SOURCE METHOD FOR CALCULATING UNSTEADY LOADS ON CAVITATING HYDROFOILSUNRUH JF; BASS RL II.1974; J. HYDRONAUT.; U.S.A.; DA. 1974; VOL. 8; NO 4; PP. 146-153; BIBL. 13 REF.Article
ENTWURF UEBERKRISTISCHER PROFILE MIT HILFE DER RHEOELEKTRISCHEN ANALOGIE. = PROJET DE PROFILS SUPER-CRITIQUES A L'AIDE DE L'ANALOGIE RHEOELECTRIQUESOBIECZKY H.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 43; PP. 1-51; ABS. ANGL.; BIBL. 2 P.Article
A COMPARISON OF TWO INTEGRAL EQUATION METHODS FOR HIGH SUBSONIC LIFTING FLOWS.NIXON D.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 1; PP. 56-58; BIBL. 2 REF.Article
ON LIFTING WINGS WITH PARABOLIC TIPS.JORDAN PF.1974; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1974; VOL. 54; NO 8; PP. 463-477; ABS. ALLEM. RUSSE; BIBL. 17 REF.Article
LIFT COEFFICIENTS ON A SUPERCAVITATING JET-FLAPPED FOIL BETWEEN RIGID WALLS.KIDA T; MIYAI Y.1975; BULL. J.S.M.E.; JAP.; DA. 1975; VOL. 18; NO 116; PP. 151-158; BIBL. 7 REF.Article
EIN NUMERISCHES VERFAHREN ZUR BERECHNUNG DER INSTATIONAEREN AERODYNAMISCHEN DRUCKVERTEILUNG DER HARMONISCH SCHWINGENDEN TRAGFLAECHE MIT RUDER IN UNTERSCHALLSTROEMUNG. THEORIE UND ERGEBNISSE FUER IKOMPRESSIBLE STROEMUNG. I. = METHODE NUMERIQUE POUR CALCULER LA DISTRIBUTION DE PRESSION AERODYNAMIQUE NON STATIONNAIRE SUR UNE AILE EN OSCILLATIONS HARMONIQUES DANS UN ECOULEMENT SUBSONIQUE. THEORIE ET RESULTATS POUR UN FLUIDE INCOMPRESSIBLE (PARTIE I)GEISSLER W.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 37; PP. 1-91; ABS. ANGL.; BIBL. 7 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
ANALYSIS OF HIGH-LIFT WING SYSTEMS.GORADIA SH; COLWELL GT.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 2; PP. 88-108; BIBL. 1 P.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
A VALIDATION STUDY OF THE MIXED-FOIL CONCEPT FOR HIGH-SPEED HYDROFOILSWANG DP; SHEN YT.1976; J. SHIP RES.; U.S.A.; DA. 1976; VOL. 20; NO 2; PP. 85-94; BIBL. 20REF.Article
TRANSONIC INVISCID FLOW OVER LIFTING AIRFOILS BY THE METHOD OF INTEGRAL RELATIONS.TSZE CHENG TAI.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 798-804; BIBL. 36 REF.Article
HYDROFOIL DEVELOPMENT. ISSUES AND ANSWERS = LA MISE AU POINT DES HYDROFOILS. QUESTIONS ET REPONSESELLSWORTH WM.sdIN: AIAA/SNAME ADV. MAR. VEH. CONF. SAN DIEGO, CALIF.; 1974; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 306; PP. 1-12; BIBL. 5 REF.Conference Paper
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
PREVISION THEORIQUE DU COMPORTEMENT LONGITUDINAL D'UN HYDROPTERE EN FORTE MERKREZELEWSKI M.1975; ZESZ. NAUK. POLITECH. GDANSK. BUDOWNICTWO OKRET.; POLSKA; DA. 1975; NO 25; PP. 1-127; ABS. ANGL. RUSSE; BIBL. 3 P. 1/2Serial Issue
THE DESIGN AND APPLICATION OF HYDROFOILS AND THEIR FUTURE PROSPECTSVON SCHERTEL BH.1974; INST. MAR. ENGRS, TRANS.; G.B.; DA. 1974; VOL. 86; NO 3; PP. 53-64; BIBL. 2 REF.Article
S3-NEW TYPE OF HIGH PERFORMANCE SEMI SUBMERGED SHIP = S3-NOUVEAU TYPE DE NAVIRE SEMI-SUBMERGE A HAUTES PERFORMANCESLANG TG.1972; J. ENGNG INDUSTRY; U.S.A.; DA. 1972; VOL. 94; NO 4; PP. 1171-1178; BIBL. 15 REF.Serial Issue