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au.\*:("CARPENTER PW")

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THE EFFECTS OF SWIRL ON THE PERFORMANCE OF SUPERCRITICAL CONVERGENT-DIVERGENT NOZZLESCARPENTER PW.1981; AERONAUT. Q.; ISSN 0001-9259; GBR; DA. 1981; VOL. 32; NO 2; PP. 126-152; BIBL. 25 REF.Article

EFFECT OF SWIRL ON THE SUBCRITICAL PERFORMANCE OF CONVERGENT NOZZLESCARPENTER PW.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 600-602; BIBL. 7 REF.Article

SMALL PERTURBATION THEORY FOR SUPERSONIC JETSCARPENTER PW.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1151; 7 P.; BIBL. 15 REF.Conference Paper

A GENERAL ONE-DIMENSIONAL THEORY OF COMPRESSIBLE INVISCID SWIRLING FLOWS IN NOZZLES.CARPENTER PW.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 3; PP. 201-216; BIBL. 12 REF.Article

A THEORETICAL INVESTIGATION OF FLOW-INDUCED INSTABILITIES IN COMPLIANT COATINGSGARRAD AD; CARPENTER PW.1982; J. SOUND VIB.; ISSN 0022-460X; GBR; DA. 1982; VOL. 85; NO 4; PP. 483-500; BIBL. 31 REF.Article

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