PARTICLE FLOWS IN SHEAR LAYERS OF EXHAUST PLUMES.BRANCH MC.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1234; PP. 1-5; BIBL. 12 REF.Conference Paper

CONSEQUENT EVENTS AS DETERMINANTS OF DRUG EFFECTS ON SCHEDULE-CONTROLLED BEHAVIOR: MODIFICATION OF EFFECTS OF COCAINE AND D-AMPHETAMINE FOLLOWING CHRONIC AMPHETAMINE ADMINISTRATIONBRANCH MC.1979; J. PHARMACOL. EXPER. THERAPEUT.; USA; DA. 1979; VOL. 210; NO 3; PP. 354-360; BIBL. 32 REF.Article

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MIXING AND REACTION OF NH₃ WITH NO IN COMBUSTION PRODUCTSBANNA SM; BRANCH MC.1981; COMBUST. FLAME; ISSN 0010-2180; USA; DA. 1981; VOL. 42; NO 2; PP. 173-181; BIBL. 21 REF.Article

CONCENTRATION VELOCITY AND PARTICLE SIZE MEASUREMENTS IN GAS-SOLID TWO-PHASE JETSHAYASHI K; BRANCH MC.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 8 P.; BIBL. 26 REF.Conference Paper

A SIMPLE MODEL OF TRANSIENT THERMAL FLAME QUENCHINGISHIKAWA N; BRANCH MC.1977; S.A.E. TRANS.; USA; DA. 1977 PUBL. 1978; VOL. 86; SECTION 3; PP. 2434-2441; BIBL. 19 REF.Article

PROPAGATION AND EXTINCTION OF COMBUSTION FRONTS IN CRUSHED OIL SHALENGUYEN K; BRANCH MC.1981; J. ENERGY RESOUR. TECHNOL.; ISSN 0195-0738; USA; DA. 1981; VOL. 103; NO 2; PP. 133-137; BIBL. 13 REF.Article

AN EXPERIMENTAL DETERMINATION OF THE QUENCHING DISTANCE OF METHANOL AND ISO-OCTANE/METHANOL BLENDS.ISHIKAWA N; BRANCH MC.1976; COMBUST. AND FLAME; U.S.A.; DA. 1976; VOL. 27; NO 1; PP. 65-72; BIBL. 10 REF.Article

A CHEMICAL KINETIC MODEL FOR THE SELECTIVE REDUCTION OF NITRIC OXIDE BY AMMONIAMILLER JA; BRANCH MC; KEE RJ et al.1981; COMBUST. FLAME; ISSN 0010-2180; USA; DA. 1981; VOL. 43; NO 1; PP. 81-98; BIBL. 44 REF.Article

A THEORETICAL INVESTIGATION OF MIXING EFFECTS IN THE SELECTIVE REDUCTION OF NITRIC OXIDE BY AMMONIABRANCH MC; KEE RJ; MILLER JA et al.1982; COMBUSTION SCIENCE AND TECHNOLOGY; ISSN 0010-2202; GBR; DA. 1982; VOL. 29; NO 3-6; PP. 147-165; BIBL. 17 REF.Article

DESIGN STUDY OF A GAS TURBINE COMBUSTOR WITH HEAT RECIRCULATION.GANJI A; BRANCH MC; OPPENHEIN AK et al.1976; IN: PROPUL. CONF. 12; PALO ALTO, CALIF.; 1976; NEW YORK; AM. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 611; PP. 1-6; BIBL. 6 REF.Conference Paper

GAS TURBINE COMBUSTOR STABILIZATION BY HEAT RECIRCULATION.GANJI AJ; SHORT J; BRANCH MC et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 6; PP. 809-812; BIBL. 7 REF.Article