Zobrazeno 1 - 10
of 112
pro vyhledávání: '"Cengiz Camci"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2018 (2018)
Three-dimensional highly complex flow structure in tip gap between blade tip and casing leads to inefficient turbine performance due to aerothermal loss. Interaction between leakage vortex and secondary flow structures is the substantial source of th
Externí odkaz:
https://doaj.org/article/6566e7b010354f54aa0edd6320d495ad
Publikováno v:
Aerospace, Vol 6, Iss 5, p 60 (2019)
Flow within the space between the rotor and stator of a turbine disk, and an area referred to as the rim seal cavity, develops azimuthal velocity component from the rotor disk. The fluid within develops unsteady structures that move at a fraction of
Externí odkaz:
https://doaj.org/article/da7e3a6589764da0ad470ed06d8cf82a
Autor:
Jason Town, Cengiz Camci
Publikováno v:
International Journal of Rotating Machinery, Vol 2015 (2015)
Five-Hole Probes (FHP), being a dependable and accurate aerodynamic tool, are an excellent choice for measuring three-dimensional flow fields in turbomachinery. To improve spatial resolution, a subminiature FHP with a diameter of 1.68 mm is employed.
Externí odkaz:
https://doaj.org/article/ec73a2a1173a4b108667ef4094605a09
Publikováno v:
International Journal of Rotating Machinery, Vol 8, Iss 2, Pp 109-123 (2002)
Externí odkaz:
https://doaj.org/article/01dc022002a440a6a8e474e7df7bfc5b
Publikováno v:
International Journal of Rotating Machinery, Vol 8, Iss 2, Pp 125-140 (2002)
Externí odkaz:
https://doaj.org/article/260205450b9d4e8785f391405ab70243
Autor:
Ali Akturk, Cengiz Camci
Publikováno v:
Journal of Aircraft. 59:233-252
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5651927c843d7cedf5958dc7fd1ec5a
https://doi.org/10.2514/1.c036386
https://doi.org/10.2514/1.c036386
Publikováno v:
Journal of Fluids Engineering. 144
It is possible to optimize a turbocharger's performance for a broad range of engine operating points. However, most of the turbochargers have distinctive performance characteristics independent of engine operation. Therefore, the correct way to obtai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6134ed06d7f71d3f7239992d447f000
https://doi.org/10.1115/1.4054466
https://doi.org/10.1115/1.4054466
Publikováno v:
SSRN Electronic Journal.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8c77d9db6180c3384e59c1bc6b852242
https://doi.org/10.2139/ssrn.4117325
https://doi.org/10.2139/ssrn.4117325
Viscous flow and performance issues in a 6:1 supersonic mixed-flow compressor with a tandem diffuser
Autor:
Aravinth Sadagopan, Cengiz Camci
Publikováno v:
Aerospace Science and Technology. 88:9-21
The advancement of multi-dimensional and viscous computational tools has eased the accessibility and overall effort for thorough analysis of complex turbomachinery designs. In this paper, we computationally evaluate a high-pressure ratio supersonic m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f345f795a39526be90c8a54c645a6a8
https://doi.org/10.1016/j.ast.2019.02.027
https://doi.org/10.1016/j.ast.2019.02.027
Autor:
Aravinth Sadagopan, Cengiz Camci
Publikováno v:
Aerospace Science and Technology. 87:265-277
A surge in the small jet engine market due to aero-propulsion purposes generates requirement to develop compact and robust high-performance compressors. We address this necessity through the design of a single-stage high-pressure ratio mixed-flow com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f5b8ca19916bca956fb204e253c6150
https://doi.org/10.1016/j.ast.2019.02.026
https://doi.org/10.1016/j.ast.2019.02.026