A methodology for robust design of impingement cooled HSCT combustor liners

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Mavris, Dimitri N ^a   Roth, Bryce ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMBUSTORS; HEAT TRANSFER; OIL WELL CASINGS; THERMAL BARRIER COATINGS; THICKNESS MEASUREMENT;

COOLING CONFIGURATION; CYCLE PARAMETERS; DESIGN PARAMETERS; DESIGN ROBUSTNESS; GENERAL METHODOLOGIES; GEORGIA INSTITUTE OF TECHNOLOGY; HIGH SPEED CIVIL TRANSPORTS; METAL TEMPERATURE;

DESIGN;

EID: 84983143210     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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6. rd Edition, John Wiley and Sons, New York, 1987.
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