Effects of exit geometry on the performance of a pulse detonation engine

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Allgood, Daniel ^a   Gutmark, Ephraim ^a   Katta, Viswanath ^b  

^a UNIVERSITY OF CINCINNATI   (United States)

^b INNOVATIVE SCIENTIFIC SOLUTIONS INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION KNOCK; EJECTORS (PUMPS); JET ENGINES;

COMPRESSION WAVES; DETONATION TUBES; DIAMETER RATIO; EJECTOR SYSTEM; PRELIMINARY ANALYSIS; THRUST AUGMENTATION;

PULSE DETONATION ENGINES;

EID: 85087602502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-613     Document Type: Conference Paper

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