Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("LIMITE")

Filter

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 225160

  • Page / 9007

Export

Selection :

  • and

ON THE SHAKEDOWN LIMIT OF A SHIP'S HULL GIRDERJONES N.1975; J. SHIP RES.; U.S.A.; DA. 1975; VOL. 19; NO 2; PP. 118-121; BIBL. 9 REF.Article

ESTIMATION DE LA VITESSE DE CONVERGENCE DANS UN THEOREME LIMITE INTEGRALBANIS II.1972; LITOV. MAT. SBOR.; S.S.S.R.; DA. 1972; VOL. 12; NO 1; PP. 41-46; ABS. LITU. ANGL.; BIBL. 5 REF.Serial Issue

BOUNDARY LAYER OVER A BLUNT BODY AT HIGH INCIDENCE WITH AN OPEN-TYPE OF SEPARATION.WANG KC.1974; PROC. R. SOC. LONDON, A; G.B.; DA. 1974; VOL. 340; NO 1620; PP. 33-55; BIBL. 19 REF.Article

A PRIORI-SCHRANKEN FUER DAS ENERGIEINTEGRAL IN EINEM RANDWERTPROBLEM MIT EINEM PARAMETER ALPHA = LIMITES A PRIORI POUR L'INTEGRALE D'ENERGIE DANS UN PROBLEME A VALEUR LIMITE AVEC UN PARAMETRE ALPHASPERB RP.1972; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1972; VOL. 23; NO 6; PP. 994-998; ABS. ANGL.; BIBL. 5 REF.Serial Issue

NONSTATIONARY ATMOSPHERIC BOUNDARY LAYER TURBULENCE SIMULATION.FICHTL GH; PERLMUTTER M.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 587; PP. (10P.); BIBL. 32 REF.Conference Paper

IMPLICIT NONITERATIVE SCHEMES FOR UNSTEADY BOUNDARY LAYERSORLANDI P; FERZIGER JH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 11; PP. 1408-1414; BIBL. 16 REF.Article

RECENT DEVELOPMENTS IN BOUNDARY-LAYER TRANSITION RESEARCH. 12TH. AEROSPACE SCIENCES MEETING; WASHINGTON, D.C.: 1974.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 3; PP. 261-314; BIBL. DISSEM.Conference Paper

DIE NUMERISCHE LOESUNG DER STATIONAEREN LAMINAREN HYPERSCHALL-GRENZSCHICHTGLEICHUNGEN BEI CHEMISCHEM NICHTGLEICHGEWICHT. = RESOLUTION NUMERIQUE DES EQUATIONS DE COUCHES LIMITES HYPERSONIQUES LAMINAIRES STATIONNAIRES DANS LE CAS DE NON EQUILIBRE CHIMIQUESCHONAUER W; STRAUB D; SPREUER H et al.1974; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 71; PP. 1-78; ABS. ANGLArticle

SUR UNE SOLUTION DES EQUATIONS DE LA COUCHE LIMITE NON STATIONNAIRE TRIDIMENSIONNELLEVERESHCHAGINA LI.1974; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1974; NO 7; PP. 102-106; ABS. ANGL.; BIBL. 3 REF.Article

THE VELOCITY AND TEMPERATURE BOUNDARY LAYERS ON A FLAT PLATE.SQUIRE W.sdIN: SYMMETRY, SIMILARITY GROUP THEOR. METHODS MECH. PROC. SYMP.; CALGARY; 1974; S.L.; DA. S.D.; PP. 359-369; BIBL. 10 REF.Conference Paper

A PHENOMENOLOGICAL DISLOCATION THEORY OF UPPER AND LOWER YIELD STRESSES OF IRONIGATA N; SETO S.1972; TRANS. IRON STEEL INST. JAP.; JAP.; DA. 1972; VOL. 12; NO 5; PP. 393-395Serial Issue

ASYMPTOTIC THEORY OF SEPARATION AND REATTACHMENT OF A LAMINAR BOUNDARY LAYER ON A COMPRESSION RAMP. = THEORIE ASYMPTOTIQUE DU DECOLLEMENT ET DU RECOLLEMENT D'UNE COUCHE LIMITE LAMINAIRE SUR UNE RAMPE DE COMPRESSIONBURGGRAF OR.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 10.1-10.9; BIBL. 11 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

COMPARISON OF TRANSITION AND FREESTREAM DISTURBANCE MEASUREMENTS OBTAINED IN TWO WIND TUNNEL FACILITIES.OWEN FK; HORSTMAN CC; STAINBACK PC et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 131; PP. 1-4; BIBL. 7 REF.Conference Paper

SUR UNE METHODE APPROCHEE DE TRAITER LA COUCHE LIMITE LAMINAIRE MAGNETOHYDRODYNAMIQUE EN REGIME NON STATIONNAIRE.ASKOVIC R.1974; ACAD. R. BELG., BULL. CL. SCI.; BELG.; DA. 1974; VOL. 60; NO 10; PP. 1261-1273; ABS. ANGL.; BIBL. 5 REF.Article

SINGULARITIES IN THREE-DIMENSIONAL TURBULENT BOUNDARY-LAYER CALCULATIONS AND SEPARATION PHENOMENACOUSTEIX J; HOUDEVILLE R.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 8; PP. 976-985; BIBL. 16 REF.Article

UPPER MASS LIMITS FOR NEUTRON STARS.HEGYI DJ; LEE TSH; COHEN JM et al.1975; ANN. NEW YORK ACAD. SCI.; U.S.A.; DA. 1975; VOL. 262; PP. 404-408; BIBL. 13 REF.; (TEXAS SYMP. RELATIVISTIC ASTROPHYS. 7; DALLAS; 1974)Conference Paper

SOLUTION D'UN PROBLEME DE CONDUCTION THERMIQUE SPATIALE POUR UN CYLINDRE SEMI-INFINI DANS DES CONDITIONS LIMITES MIXTESLIVSHITS PZ.1973; INZHENER. FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1973; VOL. 25; NO 1; PP. 160-161; BIBL. 3 REF.Serial Issue

THERMAL RESISTANCE OF TWO-DIMENSIONAL GEOMETRIES HAVING ISOTHERMAL AND ADIABATIC BOUNDARIESSCHNEIDER GE; YOVANOVICH MM.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 78; PP. 179-201; BIBL. 8 REF.Conference Paper

SIMILITUDE PROPERTIES OF HIGH-SPEED LAMINAR AND TURBULENT BOUNDARY-LAYER INCIPIENT SEPARATION.INGER GR.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 5; PP. 619-623; BIBL. 25 REF.Article

COMPUTATION OF UNSTEADY BOUNDARY LAYERS.WIRZ HJ.1975; LECTURE NOTES PHYS.; GERM.; DA. 1975; NO 41; PP. 442-476; BIBL. 3 P.; (PROGR. NUMER. FLUID DYN. LECT. SER.; RHODE-ST.-GENESE, BELG.; 1974)Conference Paper

UNTERSUCHUNGEN UEBER DAS WARMEAUSTAUSCHINTEGRAL IN TURBULENTEN, INKOMPRESSIBLEN STROEMUNGEN = ETUDE DE L'INTEGRALE DE L'ECHANGE THERMIQUE DANS DES ECOULEMENTS TURBULENTS INCOMPRESSIBLESSCHULZ JANDER B.1973; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1973; VOL. 53; NO 4; PP. 122-123; BIBL. 4 REF.; (VORTR. WISS. JAHRESTAG. GES. ANGEW. MATH. MECH.; LJUBLJANA; 1972)Conference Paper

INCOMPRESSIBLE BOUNDARY-LAYER SEPARATION.WILLIAMS JC III.1977; ANNU. REV. FLUID MECH.; U.S.A.; DA. 1977; VOL. 9; PP. 113-144; BIBL. 2 P.Article

A METHOD FOR THE CALCULATION OF 3D BOUNDARY LAYERS ON PRACTICAL WING CONFIGURATIONSLINDHOUT JPF; MOEK G; DE BOER E et al.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 1; PP. 104-111; BIBL. 14 REF.Article

UNSTEADY TURBULENT BOUNDARY LAYERS AND SEPARATION.TELIONIS DP; TSAHALIS DT.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 4; PP. 468-474; BIBL. 38 REF.Article

SOLUTION EXACTE DES EQUATIONS DE LA COUCHE LIMITE THERMIQUE POUR LES CORPS TOURNANTS A SYMETRIE AXIALE, POUR UNE REPARTITION QUELCONQUE DES TEMPERATURES DE LA SURFACEDORFMAN A SH; SELYAVIN GF.1975; TEPLOFIZ. I TEPLOTEKH., U.S.S.R.; S.S.S.R.; DA. 1975; NO 29; PP. 47-53; BIBL. 6 REF.Article

  • Page / 9007