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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

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

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

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

THE NATURE OF DIFFERENCES IN SOME FORMS OF TRANSITION IN THE BOUNDARY LAYERVOLODIN AG; ZELMAN MB.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 7; PP. 950-952; BIBL. 9 REF.Article

DREIDIMENSIONALE GRENZSCHICHTBERECHNUNGEN ENTLANG SYMMETRIELINIEN AUF KOERPERN = CALCULS DE LA COUCHE LIMITE TRIDIMENSIONNELLE LE LONG DE LIGNES DE SYMETRIE SUR DES CORPSGRUNDMANN R.1981; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1981; VOL. 5; NO 6; PP. 389-395; ABS. ENG; BIBL. 13 REF.Article

SEPARATION AHEAD OF PROTUBERANCES IN SUPERSONIC TURBULENT BOUNDARY LAYERS.SEDNEY R; KITCHENS CW JR.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 546-552; BIBL. 15 REF.Article

ON LAMINAR BOUNDARY-LAYER SEPARATION.KLINEBERG JM; STEGER JL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 94; PP. 1-17; BIBL. 2 P.Conference Paper

TURBULENT BOUNDARY-LAYER SEPARATION DUE TO A FORWARD-FACING STEP.CZARNECKI KR; JACKSON MW.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 581; PP. 1-6; H.T. 3; BIBL. 11 REF.Conference Paper

EQUATIONS UNIVERSELLES DE LA COUCHE LIMITE TRIDIMENSIONNELLE SUR UNE SURFACE CURVILIGNE PERMEABLEBOGDANOVA VV; KOZLOV LF; LISINSKAYA TI et al.1982; PRIKL. MEH. (KIEV); ISSN 0032-8243; UKR; DA. 1982; VOL. 18; NO 3; PP. 113-118; BIBL. 4 REF.Article

THE THREE DIMENSIONAL BOUNDARY LAYER ON A ROTATING HELICAL BLADEMORRIS PJ.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981-11; VOL. 112; PP. 283-296; BIBL. 8 REF.Article

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