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Roberto Claretti
Roberto Claretti
Подтвержден адрес электронной почты в домене knights.ucf.edu
Название
Процитировано
Процитировано
Год
Channel height and jet spacing effect on heat transfer and uniformity coefficient on an inline row impingement channel
M Ricklick, R Claretti, JS Kapat
Turbo Expo: Power for Land, Sea, and Air 43994, 675-684, 2010
222010
Experimental evaluation of large spacing compound angle full-coverage film cooling arrays: adiabatic film cooling effectiveness
G Natsui, R Claretti, MA Ricklick, JS Kapat, ME Crawford, G Brown, ...
Journal of Turbomachinery 138 (7), 071001, 2016
17*2016
Heat and fluid flow characterization of a single-hole-per-row impingement channel at multiple impingement heights
R Claretti
University of Central Florida, 2013
82013
Heat Transfer Study on Multiple Walls of an Impingement Channel With Variable Jet Heights
R Claretti, J Hossain, JT Harrington, JA Bernstein, SB Verma, JS Kapat
Heat Transfer Summer Conference 55492, V003T08A002, 2013
42013
Hot gas components with compound angled cooling features and methods of manufacture
BC Barr, R Claretti
US Patent 9,708,915, 2017
32017
Feasibility study of film source coupling transpiration and a row of cylindrical film holes
G Natsui, R Claretti, C Wolski, M Ricklick, JS Kapat
Turbo Expo: Power for Land, Sea, and Air 44700, 1781-1790, 2012
32012
Computational and experimental comparison of heat transfer characteristics of a triple row impingement channel at large impingement heights
R Claretti, M Ricklick, J Kapat
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6098, 2011
32011
Heat Transfer Characteristics of Jet Array Impingement at Low Streamwise Spacing
R Claretti, J Hossain, SB Verma, JS Kapat, JP Downs, GE Goebel
Turbo Expo: Power for Land, Sea, and Air 55140, V03AT12A015, 2013
22013
Experimental Evaluation of Large Spacing Compound Angle Full Coverage Film Cooling Arrays: Heat Transfer Augmentation
R Claretti, G Natsui, JS Kapat, ME Crawford, G Brown, K Landis
Heat Transfer Summer Conference 44779, 819-825, 2012
22012
Comparison of Heat Transfer and Thermal Performance of a Double Wall Cooling Scheme at Large Impingement Heights
R Claretti, M Ricklick, J Kapat
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6869, 2010
12010
Heat transfer study of a triple row impingement channel at large impingement heights
R Claretti
2011
Comparison of Heat Transfer Coefficient and Thermal Performance of a Narrow Impingement Channel
MR Ricklick, R Claretti, JS Kapat
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010
2010
Florida Turbine Technologies, Inc. Heat Transfer Division
R Claretti
Loca Heat Tranfser Characteristics of a Multi Wall Cooling Scheme at Tall Impingement Heights Using Temperature Sensitive Paint
R Claretti, M Ricklick, J Kapat
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 0
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Статьи 1–14