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kw.\*:("PERTURBATION METHOD")

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ANWENDUNG UND VERGLEICH MODALER PERTURBATIONSMETHODEN UND MODALER KORREKTURVERFAHREN AM BEISPIEL EINES PFEILFLUEGELS MIT ZWEI PYLONAUSSENLASTEN. = MODIFICATIONS DE STRUCTURE D'UNE MAQUETTE D'AILE FLECHE A DEUX CHARGES EXTERIEURES AU MOYEN DES METHODES DE PERTURBATIONS MODALES ET DE CORRECTIONS MODALESFREYMANN R.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 21; PP. 1-43; ABS. ANGL.; BIBL. 7 REF.Serial Issue

SINGULAR-PERTURBATION PROBLEMS IN SHIP HYDRODYNAMICS.OGILVIE TF.1977; ADV. APPL. MECH.; U.S.A.; DA. 1977; VOL. 17; PP. 91-188; BIBL. 4 P. 1/2Article

ON THE TWO TRIAXIAL RIGID BODY PROBLEMSIDLICHOVSKY M.1980; BULL. ASTR. INST. CZECHOSL.; CSK; DA. 1980; VOL. 31; NO 4; PP. 240-253; ABS. RUS; BIBL. 11 REF.Article

INITIAL POSTBUCKLING OF THREE-HINGED CIRCULAR ARCHSCHMIDT R.1979; J. APPL. MECH.; USA; DA. 1979; VOL. 46; NO 4; PP. 954-955; BIBL. 14 REF.Article

SMALL PERTURBATION EXPANSIONS IN UNSTEADY AEROFOIL THEORY.GRAHAM JMR; KULLAR I.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 83; NO 2; PP. 209-224; BIBL. 22 REF.Article

SISTEMATIZACION DEL METODO DE PERTURBACIONES DE A. DEPRITCAMARENA BADIA V; RIBERA PASCUAL J; PETRIZ CALVO F et al.1976; URANIA; ESP; DA. 1976; VOL. 61; NO 286; PP. 183-200; ABS. ENG; BIBL. 4 REF.Article

A RAPID METHOD FOR THE APPROXIMATE DETERMINATION OF MOLINEAR SOLUTIONS: APPLICATION TO AERODYNAMIC FLOWSSTAHARA SS; ELLIOTT JP; SPREITER JR et al.sdICAS 1980. INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES. CONGRESS. 12/1980/MUNICH; USA; DA. S.D.; PP. 324-337; BIBL. 12 REF.Conference Paper

METHODE DES PERTURBATIONS DANS LA THEORIE DU CORPS ELASTOPLASTIQUEKLYUSHNIKOV VD.1979; PRIKL. MEKH.; UKR; DA. 1979; VOL. 15; NO 8; PP. 122-123Article

UNE MODIFICATION DE LA METHODE DE HILLTITOV VB.1976; ASTR. ZH.; S.S.S.R.; DA. 1976; VOL. 53; NO 5; PP. 1100-1105; BIBL. 3 REF.Article

REFLEXION REGULIERE D'UNE PORTE ONDE DE CHOC PAR LA SURFACE D'UN COINBOGATKO VI; KOLTON GA.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 92-96; BIBL. 3 REF.Article

CORRECTING FOR RAY REFRACTION IN VELOCITY AND ATTENUATION TOMOGRAPHY: A PERTURBATION APPROACHNORTON SJ; LINZER M.1982; ULTRASON. IMAG.; ISSN 0161-7346; USA; DA. 1982; VOL. 4; NO 3; PP. 201-233; BIBL. 14 REF.Article

ON A NON-LOCAL STABILITY OF SELF-GRAVITATING STELLAR SYSTEMSTAJIMA N.1981; PROG. THEOR. PHYS.; ISSN 0033-068X; JPN; DA. 1981; VOL. 65; NO 4; PP. 1264-1280; BIBL. 13 REF.Article

INITIAL POSTBUCKLING BEHAVIOR OF UNIFORMLY COMPRESSED TWO-HINGED CIRCULAR ARCHESSCHMIDT R.1979; Z. ANGEW. MATH. MECH.; DDR; DA. 1979; VOL. 59; NO 9; PP. 473-474; BIBL. 14 REF.Article

BUCKLING OF A HEAVY LAMINA BY AN EDGE DISPLACEMENTWANG CY.1983; INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES; ISSN 0020-7403; GBR; DA. 1983; VOL. 25; NO 6; PP. 447-453; BIBL. 3 REF.Article

SMALL DISTURBANCE TRANSONIC FLOW COMPUTATION, COMBINED WITH A FULL POTENTIAL CODELUNTZ A.1982; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 24/1982-02-17/TEL-AVIV, HAIFA; ISR; HAIFA: IMPR. AYALON OFFSET; DA. 1982; PP. 204-207; BIBL. 6 REF.Conference Paper

LOW-FREQUENCY AND SMALL PERTURBATION EQUATION FOR TRANSONIC FLOW PAST WINGSCHAKRABARTTY SK; SUBRAMANIAN NR.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 9; PP. 1147-1149; BIBL. 6 REF.Article

SLIGHTLY CURVED OR KINKED CRACKSCOTTERELL B; RICE JR.1980; INT. J. FRACT.; ISSN 0376-9429; NLD; DA. 1980; VOL. 16; NO 2; PP. 155-169; ABS. FRE; BIBL. 29 REF.Article

METHODE DE ENCKE GENERALISEE POUR L'ETUDE DU MOUVEMENT PERTURBEBATRAKOV YU V; MAKAROVA EN.1979; BJULL. INST. TEOR. ASTR.; SUN; DA. 1979; VOL. 14; NO 7; PP. 397-401; ABS. ENG; BIBL. 3 REF.Article

METHODE DES PERTURBATIONS APPLIQUEE A L'ANALYSE LIMITE D'UN MILIEU GRANULAIRESZYPCIO Z; KWIECINSKI M.1978; ARCH. INZYNIER. LAD.; POLSKA; DA. 1978; VOL. 24; NO 2; PP. 257-276; ABS. RUSSE ANGL.; BIBL. 8 REF.Article

A UNIFIED APPROACH TO QUASI-STATIC SHAKEDOWN PROBLEMS OR ELASTIC-PLASTIC SOLIDS WITH PIECEWISE LINEAR YIELD SURFACEPOLIZZOTTO C.1978; MECCANICA; ITA; DA. 1978; VOL. 13; NO 2; PP. 109-120; ABS. ITA; BIBL. 24 REF.Article

MODIFIED PERTURBATION METHOD FOR THE DAMPED HARMONIC OSCILLATOR IN QUANTUM LASER THEORYZHANG LAI SHUN.1983; PHYSICA A. THEORETICAL AND STATISTICAL PHYSICS; ISSN 0378-4371; NLD; DA. 1983; VOL. 117; NO 2-3; PP. 355-368; BIBL. 17 REF.Article

A CRITICAL STUDY OF POSTBUCKLING ANALYSES OF UNIFORMLY COMPRESSED RINGSSCHMIDT R.1979; Z. ANGEW. MATH. MECH.; DDR; DA. 1979; VOL. 59; NO 10; PP. 581-582; BIBL. 21 REF.Article

COMPUTATION OF THE VIBRATIONAL MODES FOR PIEZOELECTRIC ARRAY TRANSDUCERS USING A MIXED FINITE ELEMENT PERTURBATION METHODBOUCHER D; LAGIER M; MAERFELD C et al.1981; IEEE TRANS. SONICS ULTRASON.; ISSN 0018-9537; USA; DA. 1981; VOL. 28; NO 5; PP. 318-330; BIBL. 30 REF.Article

SHAPE OF A SAIL IN A FLOWVANDEN BROECK JM; KELLER JB.1981; PHYS. FLUIDS; ISSN 0031-9171; USA; DA. 1981; VOL. 24; NO 3; PP. 552-553; BIBL. 4 REF.Article

NORMAL MODES OF ROTATING FLUIDSSOBOUTI Y.1980; ASTRON. ASTROPHYS. (BERL.); ISSN 0004-6361; DEU; DA. 1980; VOL. 89; NO 2; PP. 314-335; BIBL. 33 REF.Article

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