Pascal and Francis Bibliographic Databases

Help

Search results

Your search

au.\*:("ROM J")

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

Origin

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

Results 1 to 25 of 29

  • Page / 2
Export

Selection :

  • and

FLOWS WITH STRONG INTERACTION BETWEEN THE VISCOUS AND INVISCID REGIONS.ROM J.1975; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1975; VOL. 29; NO 2; PP. 309-328; BIBL. 2 P.Article

Ces paquebots qui vont revenir au port d'AnversROM, J.Hinterland. 1995, Num 167, pp 12-19, issn 0773-1906Article

THE CALCULATION OF NON-LINEAR AERODYNAMIC CHARACTERISTICS OF WINGS AND THEIR WAKES IN SUBSONIC FLOWZOREA CR; ROM J.1978; ISRAEL J. TECHNOL.; ISR; DA. 1978; VOL. 16; NO 1-2; PP. 83-96; BIBL. 32 REF.Conference Paper

IMPROVED FLEXIBLE SUPERSONIC WIND-TUNNEL NOZZLE OPERATED BY A SINGLE JACKROM J; ETSION I.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1697-1699; BIBL. 6 REF.Serial Issue

EFFECTS OF CHEMICAL REACTIONS ON THE PERFORMANCE OF GAS DYNAMIC LASERS.ROM J; STRICKER J.1974; ACTA ASTRONAUT.; G.B.; DA. 1974; VOL. 1; NO 7-8; PP. 1101-1117; BIBL. 23 REF.Article

CALCULATION OF SYMMETRIC VORTEX SEPARATION AFFECTING SUBSONIC BODIES AT HIGH INCIDENCEALMOSNINO D; ROM J.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 3; PP. 398-406; BIBL. 36 REF.Article

INTERACTIVE METHOD FOR COMPUTATION OF VISCOUS FLOW WITH RECIRCULATIONBRANDEIS J; ROM J.1981; J. COMPUT. PHYS.; ISSN 0021-9991; USA; DA. 1981; VOL. 40; NO 2; PP. 396-410; BIBL. 11 REF.Article

VORTEX ROLLUP OVER AND BEHIND WINGS RELATED TO NONLINEAR AERODYNAMIC CHARACTERISTICS.ZOREA C; ROM J.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 4; PP. 193-194; BIBL. 6 REF.Article

TRANSONIC VISCOUS-INVISCID INTERACTION OVER AIRFOILS FOR SEPARATED LAMINAR OR TURBULENT FLOWSGORDON R; ROM J.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 545-552; BIBL. 26 REF.Article

THREE-LAYER INTERACTIVE METHOD FOR COMPUTING SUPERSONIC LAMINAR SEPARATED FLOWSBRANDEIS J; ROM J.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 11; PP. 1320-1327; BIBL. 14 REF.Article

A FAST RESPONSE THIN FILM WATTMETER FOR MEASUREMENTS OF CO2 LASER POWERSTRICKER J; ROM J.1972; REV. SCI. INSTRUM.; U.S.A.; DA. 1972; VOL. 43; NO 8; PP. 1168-1171; BIBL. 12 REF.Serial Issue

ASSESSING THE IMPORTANCE OF INDEPENDENT VARIABLES IN NONLINEAR CAUSAL LAWSDARLINGTON R. B; ROM J. F.AMERICAN EDUCATIONAL RESEARCH JOURNAL. 1972, Vol 9, Num 3, pp 449-462Article

A METHOD FOR CALCULATING LONGITUDINAL CHARACTERISTICS OF WINGS AND MULTIPLE LIFTING SURFACES IN SUBSONIC FLOW, AND AT HIGH ANGLES OF ATTACKALMOSNINO D; ZOREA C; ROM J et al.1978; ISRAEL J. TECHNOL.; ISR; DA. 1978; VOL. 16; NO 3; PP. 132-141; BIBL. 15 REF.Article

A MODEL FOR THE EVALUATION OF INDUCED ROLLING MOMENTS AND SIDE FORCES IN SLENDER CRUCIFORM CANARD CONFIGURATIONS AT SMALL ANGLES OF INCIDENCE.GUR I; SHINAR J; ROM J et al.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 74-85; BIBL. 18 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper

LAMINAR SUPERSONIC FLOW OVER A BACKSTEP - A NUMERICAL SOLUTION AT HIGHER REYNOLDS NUMBERS.KRONZON Y; ROM J; SEGINER A et al.1976; IN: 1976 HEAT TRANSFER FLUID MECH. INST. MEET. 25. PROC.; DAVIS, CALIF.; 1976; STANFORD; UNIV. PRESS; DA. 1976; PP. 390-403; BIBL. 16 REF.Conference Paper

ON THE CALCULATION OF NON-LINEAR AERODYNAMIC CHARACTERISTICS AND THE NEAR VORTEX WAKE.ROM J; ZOREA C; GORDON R et al.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 214-228; BIBL. 1 P. 1/2Conference Paper

THE INTERACTION BETWEEN ELECTRICAL DISCHARGES AND GAS FLOW.WASSERSTROM E; CRISPIN Y; ROM J et al.1978; J. APPL. PHYS.; U.S.A.; DA. 1978; VOL. 49; NO 1; PP. 81-86; BIBL. 22 REF.Article

THE INTERACTION BETWEEN ELECTRICAL DISCHARGES AND GAS FLOW.WASSERSTROM E; CRISPIN Y; ROM J et al.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 315; PP. 1-7; BIBL. 22 REF.Conference Paper

HEAT TRANSFER IN SEPARATED REGIONS IN SUPERSONIC AND HYPERSONIC FLOWSROM J; SEGINER A; ARIELY R et al.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 14; PP. 1-12; BIBL. 1 P.1/2Conference Paper

Calculation of nonlinear subsonic characteristics of wings with thickness and camber at high incidenceGORDON, R; ROM, J.AIAA journal. 1985, Vol 23, Num 6, pp 817-825, issn 0001-1452Article

Stability of hypersonic reacting stagnation flow of a detonatable gas mixture by dynamical systems analysisTIVANOV, G; ROM, J.Combustion and flame. 1995, Vol 103, Num 4, pp 311-327, issn 0010-2180Article

CONSIDERATIONS FOR THE DESIGN OF A SECOND GENERATION INDUCTION DRIVEN TRANSONIC WIND TUNNEL.BRAHA J; SALOMON M; SEGINER A et al.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 12; PP. 729-735; BIBL. 17 REF.Article

Experimental and nonlinear vortex lattice method results for various wing-canard configurationsROM, J; MELAMED, B; ALMOSNINO, D et al.Journal of aircraft. 1993, Vol 30, Num 2, pp 207-212, issn 0021-8669Conference Paper

Interaktionen zwischen Tumorantigen-reaktiven T-Zellen des Knochenmarks und Tumorzellen bei Patientinnen mit Mammakarzinom = Interaction between tumorantigen-reactive T-cells of bone marrow and tumor cells in patients with breast cancerSCHÜTZ, F; BECKHOVE, P; FEUERER, M et al.Geburtshilfe und Frauenheilkunde. 2006, Vol 66, Num 11, pp 1059-1065, issn 0016-5751, 7 p.Article

PROCEEDINGS: SHOCK TUBES AND WAVES/12TH INTERNATIONAL SYMPOSIUM ON SHOCK TUBES AND WAVES, JERUSALEM, JULY 16-19, 1979LIFSHITZ A ED; ROM J ED.1980; SHOCK TUBES AND WAVES. INTERNATIONAL SYMPOSIUM ON SHOCK TUBES AND WAVES. 12/1979-07-16/JERUSALEM; ISR; JERUSALEM: MAGNES PRESS/JERUSALEM: HEBREW UNIVERSITY; DA. 1980; 735 P.; 26 CM; ISBN 965-223-350-1Conference Proceedings

  • Page / 2