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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

ETUDE PAR VISUALISATIONS HYDRODYNAMIQUES, DE DIVERS PROCEDES DE CONTROLE D'ECOULEMENTS DECOLLES.WERLE H; GALLON M.1976; RECH. AEROSPAT.; FR.; DA. 1976; NO 2; PP. 75-94; ABS. ANGL.; BIBL. 34 REF.Article

THIN-AIRFOIL THEORY OF AN EJECTOR-FLAPPED WING SECTION.WOOLARD HW.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 187; PP. 1-11; BIBL. 9 REF.Conference Paper

LE MARCHE FRANCAIS DES VOLETS ROULANTS.LEGRAND JC.1977; CHARP. MENUIS. METAL. SERRUR.; FR.; DA. 1977; NO 99; PP. 30-31Article

AERODYNAMICS OF INVERTED LEADING-EDGE FLAPS ON DELTA WINGSMARCHMAN JF III.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 12; PP. 1051-1056; BIBL. 5 REF.Article

THE TRANSONIC OSCILLATING FLAP.MAGNUS R; YOSHIHARA H.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 327; PP. 1-13; BIBL. 8 REF.Conference Paper

NUMERICAL CALCULATION OF THE COMPRESSIBLE FLOW OVER AN AIRFOIL WITH A JET FLAP.IVES DC; MELNIK RE.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 542; PP. 1-14; BIBL. 14 REF.Conference Paper

STOL ENGINE SYSTEMS AND SENSITIVITY FACTORSGODSTON J.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1644-1653; BIBL. 22 REF.Serial Issue

HYPERSONIC FLOW OVER SMALL SPAN FLEPS IN A THICK TURBULENT BOUNDARY LAYERCASSEL LA; JARRETT TW.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; PP. 137-166; BIBL. 16 REF.Conference Paper

ANALYSIS OF UNSTEADY PRESSURE MEASUREMENTS ON AN AEROFOIL SECTION WITH AN HARMONICALLY OSCILLATING, SLOTTED FLAPKIENAPPEL KARL; ROUND DAVID F.1980; D.F.V.L.R. FORSCH.-BER.; DEU; DA. 1980; VOL. 80; NO 22; 65 P.; ABS. GER; BIBL. 1 REF.Serial Issue

MOTORISATION ET COMPENSATION: POUR OU CONTRE LA COMPENSATION AVEC LA MOTORISATION.1977; CHARP. MENUIS. METAL. SERRUR.; FR.; DA. 1977; NO 97; PP. 43-45Article

PROPULSION CHARACTERISTICS AFFECTING THE AERODYNAMIC PERFORMANCE OF AN EXTERNALLY BLOWN FLAP TRANSPORT MODEL.HOAD DR.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1218; PP. 1-4; H.T. 3; BIBL. 14 REF.Conference Paper

HYBRID UPPER SURFACE BLOWN FLAP PROPULSIVE-LIFT CONCEPT FOR THE QUIET SHORT-HAUL RESEARCH AIRCRAFT.COCHRANE JA; CARROS RJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1220; PP. 1-8; BIBL. 5 REF.Conference Paper

EN ANGLAISHALSEY ND.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 188; PP. 1-11; BIBL. 19 REF.Conference Paper

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

LIFT AND DRAG CHARACTERISTICS OF A SUPERCAVITATING CAMBERED HYDROFOIL WITH A JET FLAP BENEATH A FREE SURFACE.TAKE T; KIDA T.1976; BULL. J. S.M.E.; JAP.; DA. 1976; VOL. 19; NO 130; PP. 377-383; BIBL. 13 REF.Article

DAS FENSTERBAUER-KOMPLETTFENSTER MIT SCHALLSCHUTZ-ROLLADEN-ELEMENTEN VON PAUL = ENSEMBLE FENETRES-VOLETS ROULANTS A HAUTE ISOLATION ACOUSTIQUE DE LA FIRME PAUL1979; GLAS+RAHMEN; DEU; DA. 1979; VOL. 30; NO 12; PP. 648-650; (2 P.)Article

WIND TUNNEL TESTS OF A SLOTTED FLAPPED WING SECTION.MARSDEN DJ.1978; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1978; VOL. 24; NO 2; PP. 83-91; BIBL. 8 REF.Article

EVALUATION OF A NEW JET FLAP PROPULSIVE-LIFT SYSTEM.YA TUNG CHIN; AIKEN TN; OATES GS JR et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 605-610; BIBL. 6 REF.Article

RATIONAL FUNCTION REPRESENTATION OF FLAP NOISE SPECTRA INCLUDING CORRECTION FOR REFLECTION EFFECTS.MILES JH.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 193; PP. 1-24; H.T. 6; BIBL. 2 P. 1/2Conference Paper

NOISE RADIATION FROM THE SIDE EDGES OF FLAPSHARDIN JC.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 549-552; BIBL. 11 REF.Article

ETUDE DES EFFETS INSTATIONNAIRES DE GOUVERNE EN ECOULEMENT TRIDIMENSIONNEL SUBSONIQUE ET TRANSSONIQUECONSIGNY H.1982; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1982; NO 2; PP. 75-92; ABS. ENG; BIBL. 7 REF.Article

MESSBERICHT. III. ERMITTLUNG DES EINFLUSSER VON GESCHLOSSENEM ROLLADEN AUF DEN WARMEDURCHGANG VON FENSTERN = MEASUREMENT REPORT. III. EVALUATION OF THE INFLUENCE OF CLOSED ROLLER BLIND ON HEAT TRANSFER THROUGH THE WINDOW = COMPTE RENDU DE MESURES. III. DETERMINATION DE L'INFLUENCE DES VOLETS ROULANTS FERMES SUR L'ECOULEMENT THERMIQUE PAR LES FENETRES1978; SCHWEIZ. BL. HEIZUNG LUEFTUNG; CHE; DA. 1978; VOL. 45; NO 3; PP. 92-98Article

MESSBERICHT. IV. BESTIMMUNG DES SCHALLDAMMASSES R UND DES SCHALLISOLATIONSINDEXES IA AN VERSCHIEDENEN "FENSTER-ROLLADEN"- UND "FENSTER-STOREN"-KOMBINATIONEN. = COMPTE RENDU DE MESURES. IV. DETERMINATION DE L'AMORTISSEMENT DU BRUIT R ET DE L'INDICE D'ISOLATION PHONIQUE IA POUR DIVERSES COMBINATIONS "FENETRES-VOLETS ROULANTS" ET "FENETRES-STORES"LAUBER A.1978; SCHWEIZ. BL. HEIZUNG LUEFTUNG; CHE; DA. 1978; VOL. 45; NO 3; PP. 99-105Article

KUNSTSTOFF-ROLLAEDEN ALS SCHALLDAEMM-ELEMENTE. = LES VOLETS EN MATIERE PLASTIQUE UTILISES POUR AMELIORER L'ISOLATION ACOUSTIQUE1976; GLAS+RAHMEN; DTSCH.; DA. 1976; NO 18; PP. 672-676 (3P.)Article

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