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au.\*:("PRZIREMBEL CEG")

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AEROTHERMODYNAMIC CHARACTERISTICS OF A RESONANCE TUBE DRIVEN BY A SUBSONIC JET.PRZIREMBEL CEG; FLETCHER LS.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 2; PP. 184-186; BIBL. 6 REF.Article

AEROTHERMODYNAMIC ASPECTS OF AN AXISYMMETRIC RESONANCE TUBEPRZIREMBEL CEG.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 9; PP. 1141-1143; BIBL. 5 REF.Article

AERODYNAMICS OF SLENDER BODIES AT HIGH ANGLER OF ATTARKPRZIREMBEL CEG; SHEREDA DE.1979; J. SPACECR. ROCK.; USA; DA. 1979; VOL. 16; NO 1; PP. 10-14; BIBL. 14 REF.Article

TRANSIENT ANALYSIS OF THE AEROTHERMODYNAMIC CHARACTERISTICS OF A RESONANCE TUBEPRZIREMBEL CEG; WOLF DE; ANDRE GR et al.1979; THERMOPHYSICS CONFERENCE. 14/1979/ORLANDO FL; USA; NEW YORK: AIAA; DA. 1979; 79-1050; 8 P.; BIBL. 22 REF.Conference Paper

CINEMATOGRAPHIC STUDY OF SEPARATED FLOW REGIONS. = ETUDE CINEMATOGRAPHIQUE DES REGIONS D'ECOULEMENT DECOLLEPAGE RH; PRZIREMBEL CEG.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 38.1-38.7; BIBL. 1 P.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

AEROTHERMODYNAMICS OF A SIMPLE RESONANCE TUBE.PRZIREMBEL CEG; FLETCHER LS.1977; A. I.A.A., J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 1; PP. 101-104; BIBL. 31 REF.Article

THERMODYNAMIC CHARACTERISTICS OF A BLUNT TWO-DIMENSIONAL RESONANCE TUBE.PRZIREMBEL CEG; FLETCHER LS; WOLF DE et al.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 7; PP. 905-906; BIBL. 4 REF.Article

THE EFFECT OF BASE MOUNTED CYLINDERS ON A NEAR WAKEMERZ RA; PAGE RH; PRZIREMBEL CEG et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-7; BIBL. 17 REF.Conference Paper

SUBSONIC AXISYMMETRIC NEAR-WAKE STUDIESMERZ RA; PAGE RH; PRZIREMBEL CEG et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 656-662; BIBL. 25 REF.Article

MODIFICATION OF SUBSONIC WAKES USING BOUNDARY LAYER AND BASE MASS TRANSFERPORTEIRO JLF; PRZIREMBEL CEG; PAGE RH et al.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 665-670; BIBL. 15 REF.Article

REAR STAGNATION POINT LOCATION IN A SUBSONIC NEAR-WAKE.MERZ RA; PAGE RH; PRZIREMBEL CEG et al.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 319-320; BIBL. 5 REF.Article

GENERALIZED FLOW ACROSS AN ABRUPT ENLARGEMENT.BENEDICT RP; WYLER JS; DUDEK JA et al.1976; J. ENGNG POWER; U.S.A.; DA. 1976; VOL. 98; NO 3; PP. 327-334; BIBL. 36 REF.Article

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