SELECTION OF THE OPTIMAL DEGREE OF REACTION OF THE STAGES OF A GAS TURBINE WITH UNSHROUDED BLADES.
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Pagination or Media Count:
There are presented the results of computational investigations for determining the optimal degree of reaction for the stages of gas turbines with unshrouded guiding and operating blades. The work was carried out on the electronic computer Ural-l. The results are compared with the experimental data. Author
- Jet and Gas Turbine Engines