Zobrazeno 1 - 10
of 19
pro vyhledávání: '"D. G. Lilley"'
Publikováno v:
ASME 1994 International Computers in Engineering Conference and Exhibition.
A computer code has been developed to simulate the turbulent combustion flowfield of an axisymmetric swirling flow in a typical combustor. Fuel enters centrally through a round cross-sectioned inlet while air enters through a concentric annular injet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ffc26822acbe94586f84ae759ddf7cd0
https://doi.org/10.1115/cie1994-0462
https://doi.org/10.1115/cie1994-0462
Autor:
T.-K. Lin, D. G. Lilley
Publikováno v:
ASME 1994 International Computers in Engineering Conference and Exhibition.
The development, use and application of a three-dimensional fluid flow computer code is described. The code runs on microcomputers with effective 3-D perspective color graphic displays of the results. The present version of the code retains several s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::818bb114fc327dc82e5ebd9ad6ba1a88
https://doi.org/10.1115/cie1994-0458
https://doi.org/10.1115/cie1994-0458
Autor:
A. S. Halal, D. G. Lilley
Publikováno v:
28th Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6cf243149880d7e3387fb69f6d1468aa
https://doi.org/10.2514/6.1990-154
https://doi.org/10.2514/6.1990-154
Publikováno v:
Journal of Energy. 3:95-105
In order to complement associated experimental studies, the development of a theoretical approach to the evaluation of gas turbine combustors is extremely attractive. For this purpose a computer program is needed which starts from hypotheses about th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c450532257feb40b994511f9bae3b0f9
https://doi.org/10.2514/3.62416
https://doi.org/10.2514/3.62416
Publikováno v:
Journal of Fluids Engineering. 104:378-384
Combustor modeling has reached the stage where the most useful research activities are likely to be on specific sub-problems of the general three-dimensional turbulent reacting flow problem. The present study is concerned with a timely fluid dynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4274b6f7fe1a992a19b49e7a5312577
https://doi.org/10.1115/1.3241855
https://doi.org/10.1115/1.3241855
Publikováno v:
17th Aerospace Sciences Meeting.
Complementary to the lengthy and costly experimental approach to gas turbine combustor development is the theoretical approach. In order to advance the combustor design process, a computer program is needed which starts from hypotheses about the fund
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::80f5846c4a5a691d9f4081cd43c8a19e
https://doi.org/10.2514/6.1979-354
https://doi.org/10.2514/6.1979-354
Autor:
J. W. Samples, D. G. Lilley
Publikováno v:
22nd Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bba81e80711157131b98fe6a03c9f588
https://doi.org/10.2514/6.1984-364
https://doi.org/10.2514/6.1984-364
Autor:
D. G. Lilley, G. B. Ferrell
Publikováno v:
21st Joint Propulsion Conference.
Experiments have been conducted to characterize the time-mean and turbulent flowfield of a deflected turbulent jet in a confining cylindrical crossflow. Jet-to-crossflow velocity ratios of 2, 4, and 6 were investigated, with no swirl in the crossflow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82e4a5757090d54b4dba8f59813de281
https://doi.org/10.2514/6.1985-1102
https://doi.org/10.2514/6.1985-1102
Autor:
D. G. Lilley, H. K. Yoon
Publikováno v:
21st Aerospace Sciences Meeting.
Nonswirling and swirling nonreacting flows in an axisymmetric test section with an expansion ratio D/d = 2, which may be equipped with contraction nozzles of area ratios 2 and 4, are investigated. The effects of a number of geometric parameters on th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::be3cb5ffc1e90da8612e46a94fac49a0
https://doi.org/10.2514/6.1983-315
https://doi.org/10.2514/6.1983-315
Publikováno v:
17th Joint Propulsion Conference.
Numerical computations have been undertaken for a basic two-dimensional axisymmetric flowfield which is similar to that found in conventional gas turbine and ramjet combustors. A swirling flow enters a larger chamber via a sudden or gradual expansion
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53ef4c5c1f502540c9593bac68b8c5fc
https://doi.org/10.2514/6.1981-1485
https://doi.org/10.2514/6.1981-1485