Article
Licensed
Unlicensed
Requires Authentication
Overall Performance Measurements of Annular Combusts Used in P-60 Miniature Turbojet Engine
-
Bor-Jang Tsai,
Published/Copyright:
September 1, 1999
Published Online: 1999-09
©2011 by Walter de Gruyter GmbH & Co.
You are currently not able to access this content.
You are currently not able to access this content.
Articles in the same Issue
- CONTENTS
- Intelligent Control for the Main Fuel Flow of the F-100 Turbofan Engine
- A General Variational Theory Of Multipoint Inverse Design Of 2-D Transonic Cascades Based On An Artificial Flow-Oscillation Model
- Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor
- Effect of Gear Tooth Imperfection on Dynamics of Gear Transmission Systems
- Overall Performance Measurements of Annular Combusts Used in P-60 Miniature Turbojet Engine
Articles in the same Issue
- CONTENTS
- Intelligent Control for the Main Fuel Flow of the F-100 Turbofan Engine
- A General Variational Theory Of Multipoint Inverse Design Of 2-D Transonic Cascades Based On An Artificial Flow-Oscillation Model
- Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor
- Effect of Gear Tooth Imperfection on Dynamics of Gear Transmission Systems
- Overall Performance Measurements of Annular Combusts Used in P-60 Miniature Turbojet Engine
