INTERNATIONAL JOURNAL OF TURBO AND JET ENGINES

 

VOL. 18, NO. 1, 2001

 

The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine

Daniel J. Dorney, Horia C. Flitan, David E. Ashpis, William J. Solomon.......................................................................... 1

 

Effects of Hot Streak Shape on Rotor Heating in a High-Subsonic Single-Stage Turbine

Daniel J. Dorney and Karen L. Gundy-Burlet...................................................................................................................... 15

 

A Simple Method for Geometry Definition of Radial Compressors

V.Zurita-Ugalde, J.C. Gomez-Mancilla, F.Garcia-Cristiano................................................................................................ 31

 

Advanced Aerothermodynamics Associated with Clean Technologies for Upgrading Gas Turbines in Simple and Combined-Cycle Power Stations

Benjamin Gal-Or....................................................................................................................................................................... 37

 

Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety

Benjamin Gal-Or....................................................................................................................................................................... 41

 

Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material

Zhen-Xue Han, Brian H. Dennis, George S. Dulikravich................................................................................................... 47

 

A Simple Mobile Anechoic Chamber For Experiments in Jet Acoustics

K. Srinivasan and E. Rathakrishnan..................................................................................................................................... 59

 

The Influence of Fuel Droplet Characteristics on Chemical Mechanisms in a Premixed Laminar Spray Flame

J.B. Greenberg and A. Kalma................................................................................................................................................. 65