A preliminary shape design for axial gas-turbine blade
碩士 === 逢甲大學 === 機械工程研究所 === 75 ===
Main Authors: | WU, RONG-HE, 吳榮和 |
---|---|
Other Authors: | ZHANG, XUE-BIN |
Format: | Others |
Language: | zh-TW |
Published: |
1987
|
Online Access: | http://ndltd.ncl.edu.tw/handle/26465848285297188950 |
Similar Items
-
FREE VIBRATIONS OF GAS TURBINE ENGINE AXIAL COMPRESSOR BLADES
by: Михаил Романович Ткач, et al.
Published: (2020-08-01) -
A design method for the prediction of unsteady forces on subsonic, axial gas-turbine blades
by: Korakianitis, Theodosios P. (Theodosios Prokopios)
Published: (2005) -
Implicit geometric representation of gas turbine blades for optimal shape design
by: Mansour, Tarek
Published: (2005) -
An improved axial-flow siren for fatigue testing gas turbine blades
by: Donnelly, Thomas Francis, et al.
Published: (2012) -
Profitability of the gas-turbine engine with two-row blade wreaths in the axial compressor
by: П.І. Греков, et al.
Published: (2005-04-01)