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NONLINEAR AERODYNAMIC MODELING OF FLAP OSCILLATIONS IN TRANSONIC FLOW: A NUMERICAL VALIDATIONCHYU WJ; SCHIFF LB.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 106-113; BIBL. 16 REF.Article

IMPROVED FINITE-DIFFERENCE SCHEME FOR TRANSONIC AIRFOIL FLOWFIELD CALCULATIONSLEE TZONG CHEN.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 2; PP. 218-226; BIBL. 19 REF.Article

CW LONGITUDINAL MODE SPECTRA OF MULTIPLE QUANTUM WELL STRIPE LASERSLINDSTROEM C; HALIDO D; SCIFRES DR et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 876-878; BIBL. 15 REF.Article

DUAL-WAVELENGTH (GAAL) AS LASERBOUADMA N; BOULEY JC; RIOU J et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 871-873; BIBL. 5 REF.Article

IN GAASP/INP (1.3 MU M) BURIED-CRESCENT LASERS WITH SEPARATE OPTICAL CONFINEMENTLOGAN RA; VAN DER ZIEL JP; TEMKIN H et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 895-896; BIBL. 5 REF.Article

HIGHER-ACCURACY FINITE-DIFFERENCE SCHEMES FOR TRANSONIC AIRFOIL FLOWFIELD CALCULATIONSLEE TZONG CHEN.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 9 P.; BIBL. 19 REF.Conference Paper

NUMERYCZNA ANALIZA PEWNYCH ZAGADNIEN HYDROSPREZYSTOSCI = ANALYSE NUMERIQUE DE PROBLEMES PARTICULIERS DE L'HYDROELASTICITESZMIDT K.1981; ARCH. HYDROTECH.; ISSN 0004-0789; POL; DA. 1981; VOL. 28; NO 1; PP. 3-22; ABS. RUS/ENG; BIBL. 12 REF.Article

RINGS THAT ARE NEARLY ASSOCIATIVEZHEVLAKOV KA; SLIN'KO AM; SHESTAKOV IP et al.1982; PURE APPL. MATH.; ISSN 508268; USA; DA. 1982; NO 104; 371 P.; BIBL. 284 REF.Article

SINGULARITIES OF SETS USED IN THE MESH METHODSYCZEWSKI M; TRIBILLO R.1981; COMPUT. STRUCT.; ISSN 0045-7949; USA; DA. 1981; VOL. 14; NO 5-6; PP. 509-511; BIBL. 11 REF.Article

A BROADCAST PROTOCOL FOR FILE TRANSFERS TO MULTIPLE SITESCALO SB; EASTON MC.1981; IEEE TRANS. COMMUN.; ISSN 0090-6778; USA; DA. 1981; VOL. 29; NO 11; PP. 1701-1707; BIBL. 5 REF.Article

VERTICAL DIFFERENCING OF THE PRIMITIVE EQUATIONS IN SIGMA COORDINATESARAKAWA A; SUAREZ MJ.1983; MONTHLY WEATHER REVIEW; ISSN 0027-0644; USA; DA. 1983; VOL. 111; NO 1; PP. 34-45; BIBL. 10 REF.Article

ON A MULTI-TIME STEP PROCEDURE TO ACCELERATE TIME-ASYMPTOTIC FLOW CALCULATIONSSEDIN YCJ.1982; CONFERENCE ON NUMERICAL METHODS IN FLUID MECHANICS. 4/1981/PARIS; DEU; BRAUNSCHWEIG; WIESBADEN: F. VIEWEG; DA. 1982; PP. 301-310; BIBL. 2 REF.Conference Paper

RADIATIVE TRANSFER: ANALYTIC SOLUTION OF DIFFERENCE EQUATIONSKALKOFEN W; WEHRSE R.1982; ASTRON. ASTROPHYS. (BERL.); ISSN 0004-6361; DEU; DA. 1982; VOL. 108; NO 1; PP. 42-48; BIBL. 11 REF.Article

ROOM-TEMPERATURE CW OPERATION OF 1.3 MU M DISTRIBUTED-FEEDBACK GAIN ASP/INP LASERSUEMATSU Y; OKUDA H; KINOSHITA J et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 857-858; BIBL. 3 REF.Article

VERY LOW THRESHOLD GRIN-SCH GAAS/GA ALAS LASER STRUCTURE GROWN BY OM-VPEHERSEE SD; BALDY M; ASSENAT P et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 870-871; BIBL. 7 REF.Article

ISOPARAMETRIC FINITE DIFFERENCE ENERGY METHOD FOR PLATE BENDING PROBLEMSBARVE VD; DEY SS.1983; COMPUTERS & STRUCTURES; ISSN 0045-7949; USA; DA. 1983; VOL. 17; NO 3; PP. 459-465; BIBL. 13 REF.Article

STOCHASTIC DIFFERENTIAL EQUATIONS ON MANIFOLDSELWORTHY KD.1982; LECT. NOTE SER.-LONDON MATH. SOC.; ISSN 0076-0552; GBR; DA. 1982; VOL. 70; 325 P.; BIBL. 11 P.Serial Issue

FINITE DIFFERENCE REPRESENTATIONS OF VORTICITY TRANSPORTJOSEPH M.1983; COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING; ISSN 0045-7825; NLD; DA. 1983; VOL. 39; NO 2; PP. 107-116; BIBL. 39 REF.Article

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

TRANSONIC FLOW CALCULATIONS USING THE EULER EQUATIONSATKINS HL; HASSAN HA.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 6; PP. 842-847; BIBL. 17 REF.Conference Paper

MERIDIONAL FLOW CALCULATIONS USING A FINITE DIFFERENCE METHODBOSMAN C; MANCHESTER U.1982; NUMERICAL METHODS FOR FLOWS IN TURBOMACHINERY BLADINGS. COURSE/1982/RHODE-SAINT-GENESE; BEL; RHODE-SAINT-GENESE: VON KARMAN INSTITUTE FOR FLUID DYNAMICS; DA. 1982; VOL. 2; PP. 1-32Conference Paper

REASSESSMENT OF SOLUTIONS OF FINITE DIFFERENCE EQUATIONS IN FLUID MECHANICSTAL R.1982; LETT. HEAT MASS TRANSFER; ISSN 0094-4548; USA; DA. 1982; VOL. 9; NO 3; PP. 227-229; BIBL. 3 REF.Article

SHORT-CAVITY GAALAS LASER BY WET CHEMICAL ETCHINGBOUADMA N; RIOU J; BOULEY JC et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 879-880; BIBL. 8 REF.Article

CURRENT/FREQUENCY-MODULATION CHARACTERISTICS FOR DIRECTLY OPTICAL FREQUENCY-MODULATED INJECTION LASERS AT 830 NM AND 1.3 MU MJACOBSEN G; OLESEN H; BIRKEDAHL F et al.1982; ELECTRONICS LETTERS; ISSN 0013-5194; GBR; DA. 1982; VOL. 18; NO 20; PP. 874-876; BIBL. 7 REF.Article

LAMINARE GRENZSCHICHTEN IN DER NAEHE DER ANLEGELINIE AN FLUEGELN UND FLUEGELAEHNLICHEN KOERPERN MIT ANSTELLUNG = COUCHES LIMITES LAMINAIRES AU VOISINAGE DE LA LIGNE DE CONTACT SUR DES AILES ET D'AUTRES CORPS SEMBLABLES EN INCIDENCESCHWAMBORN D.1981; DTSCH. LUFT-RAUMFAHRT, FORSCHUNGSBER; ISSN 0070-4245; DEU; DA. 1981; NO 31; 157 P.; ABS. ENG; BIBL. 44 REF.Serial Issue

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