kw.\*:("TANGAGE")
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METHODS FOR ESTIMATING VEHICLE TRANSFER FUNCTIONS REQUIRING ONLY THE GEOMETRIC AND INERTIA CHARACTERISTICSHUMPHREYS DE; WATKINSON KW.1972; IN: OCEAN 72 IEEE INT. CONF. ENG. OCEAN ENVIRON. REC. NEWPORT, R.I., 1972; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1972; PP. 220-223; BIBL. 4 REF.Conference Proceedings
OCEAN CATAMARAN SEAKEEPING DESIGN, BASED ON THE EXPERIENCES OF USNS HAYES = CONCEPTION DE LA TENUE EN MER DE CATAMARANS OCEANIQUES, EN SE FONDANT SUR L'EXPERIENCE DU USNS HAYESHADLER JB; LEE CM; BIRMINGHAM JT et al.1974; SOC. NAV. ARCHITECTS MAR. ENGRS, TRANS.; U.S.A.; DA. 1974; VOL. 82; PP. 126-161; BIBL. 41REF.Article
VIKING CONFIGURATION PITCH DAMPING DERIVATIVES AS INFLUENCED BY SUPPORT INTERFERENCE AND TEST TECHNIQUE AT TRANSONIC AND SUPERSONIC SPEEDS = L'INFLUENCE DE L'INTERFERENCE DU SUPPORT SUR LA MESURE DES DERIVEES DE TANGAGE DANS LA CONFIGURATION VIKING ET LA TECHNIQUE D'ESSAI AUX VITESSES TRANSONIQUES ET SUPERSONIQUESSTEINBERG S; USELTON BL; SIEMERS PM III et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-9; BIBL. 16 REF.Conference Paper
THEORIE ASYMPTOTIQUEMENT LINEAIRE DU TANGAGE D'UN NAVIRE EN EAU PROFONDEVOROB'EV YU L.1975; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1975; VOL. 11; NO 11; PP. 106-112; BIBL. 8REF.Article
COMPARISON OF THREE OSCILLATORY TECHNIQUES FOR CONES AT INCIDENCE = COMPARAISON DE TROIS TECHNIQUES OSCILLATOIRES POUR DES CONES EN INCIDENCEORLIK RUCKEMANN KJ; IYENGAR S; LABERGE JG et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-7; BIBL. 9 REF.Conference Paper
WIND-TUNNEL MEASUREMENT OF DYNAMIC CROSS-COUPLING DERIVATIVES.HANFF ES; ORLIK RUCKEMANN J.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 1; PP. 40-46; BIBL. 7 REF.Article
MESURES A GRANDE ECHELLE PENDANT UNE GRANDE DUREE SUR UN BATEAU DE CONTENEURSTAKAHASHI Y; OBATA K; NOSE Y et al.1983; JOURNAL OF THE SOCIETY OF NAVAL ARCHITECTS OF JAPAN; ISSN 0514-8499; JPN; DA. 1983; VOL. 152; PP. 268-274; ABS. ENG; BIBL. 6 REF.Article
HYDRODYNAMIC POWER RADIATED BY A HEAVING AND PITCHING AIR-CUSHION VEHICLE.DOCTORS LJ.1978; J. SHIP RES.; USA; DA. 1978; VOL. 22; NO 2; PP. 67-69; BIBL. 18 REF.Article
MOUVEMENTS D'UN BATEAU PLANANT A GRANDE VITESSE DANS UNE MER REGULIEREBESSHO M; KOMATSU M; ANJOH M et al.1974; J. SOC. NAV. ARCHITECTS JAP.; JAP.; DA. 1974; VOL. 135; PP. 109-120; ABS. ANGL.; BIBL. 9 REF.Article
EMPIRICAL ESTIMATES OF GUST LOADS ON FINITE WINGSPATEL MH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 12; PP. 1602-1604; BIBL. 7 REF.Article
EFFECTS OF REYNOLDS NUMBER ON SWEPT-WING-BODY CONFIGURATIONS WITH HIGH LIFT DEVICES AT TRANSONIC SPEEDS.ATRAGHJI E; SORENSEN H.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 94-120; BIBL. 8 REF.Conference Paper
REPONSE AU CLAQUEMENT ET DEFAILLANCE DE LA STRUCTURE D'UN PETIT NAVIREYAMAMOTO Y; OHTSUBO H; TAKEDA Y et al.1981; J. SOC. NAV ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1981; VOL. 149; NO 6; PP. 134-139; ABS. ENG; BIBL. 9 REF.Article
EFFECT OF INTERBLADE PHASE ANGLE AND INCIDENCE ANGLE ON CASCADE PITCHING STABILITYCARTA FO; ST HILAIRE AO.1980; J. ENGNG POWER; USA; DA. 1980; VOL. 102; NO 2; PP. 391-396; BIBL. 15 REF.Article
FORCES PERTURBATRICES LORS DU TANGAGE DU VAISSEAU DANS DES EAUX PROFONDES ET PEU PROFONDESVOROB'EV YU L.1980; PRIKL. MEKH.; UKR; DA. 1980; VOL. 16; NO 4; PP. 136-139; BIBL. 6 REF.Article
AERODYNAMIC CHARACTERISTICS OF AN AXISYMMETRIC BODY UNDERGOING A UNIFORM PITCHING MOTION.SMITH LH; NUNN RH.1976; J. SPACECR. ROCK; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 8-14; BIBL. 15 REF.Article
AERODYNAMIC CHARACTERISTICS OF AN AXISYMMETRIC BODY UNDERGOING A UNIFORM PITCHING MOTION.SMITH LH; NUNN RH.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 838; PP. 1-9; BIBL. 15 REF.Conference Paper
LIGHT HOVERCRAFT CHARACTERISTICS = CARACTERISTIQUES DE HOVERCRAFTS LEGERSWATERS D.1974; HOVERG CRAFT HYDROFOIL; G.B.; DA. 1974; VOL. 13; NO 10; PP. 20-27; BIBL. 11 REF.Article
ANALYSIS OF FLOW-REVERSAL DELAY FOR A PITCHING AIRFOIL. = ANALYSE DU RETARD DE L'INVERSION DE L'ECOULEMENT POUR UN PROFIL AERODYNAMIQUE ANIME D'UN MOUVEMENT DE TANGAGESCRUGGS RM; NASH JF; SINGLETON RE et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON, 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 183; PP. 1-11; BIBL. 24 REF.Conference Paper
NUMERICAL PREDICTION OF DYNAMIC FORCES ON ARBITRARILY PITCHED AIRFOILSHEGNA HA.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 161-162; BIBL. 7 REF.Article
UNSTEADY KUTTA CONDITION OF A PLUNGING AIRFOILHO CH; CHEN SH.1981; UNSTEADY TURBULENT SHEAR FLOWS. SYMPOSIUM ON UNSTEADY TURBULENT SHEAR FLOWS/1981/TOULOUSE; DEU/USA; BERLIN; NEW YORK: SPRINGER; DA. 1981; PP. 197-206; BIBL. 10 REF.Conference Paper
SHIP ROOL RESPONSE AND CAPSIZE BEHAVIOUR IN BEAM SEASWRIGHT JHG; MARSHFIELD WB.1980; NAV. ARCHIT.; ISSN 0306-0209; GBR; DA. 1980; NO 3; PP. 129-148; BIBL. DISSEM.Article
THE DELTA WING IN OSCILLATORY GNOTSPATEL MH.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 481-486; BIBL. 22 REF.Article
WAVE DATA REQUIREMENTS FOR SHIP DESIGN AND OPERATIONBALES SL; COMMINS WE.1979; MAR. SCI.; USA; DA. 1979; VOL. 8; PP. 93-107; BIBL. 13 REF.Article
GIDRODINAMICHESKAYA TEORIYA KACHKI KORABLYA = THEORIE HYDRODYNAMIQUE DU MOUVEMENT D'UN NAVIREKHASKIND MD.1973; MOSKVA; NAUKA; DA. 1973; PP. 1-327; BIBL. 5 P. 1/2Book
AERODYNAMIC FORCES ON FINITE WINGS IN OBLIQUE GUSTSPATEL MH.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 1; PP. 71-75; BIBL. 14 REF.Article