Objective
The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines.

The　International Journal of Turbo & Jet Engines　is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.

Topics

Turbo and jet engines
Theory and design of propagation of (advanced) jet aircraft
Thermodynamics
Combustion
Behavior of materials at High temperatures
Turbine and engine design
Thrust vectoring or Jet-Engine-Steering in effecting improved Flight control
Energy and environmental issue
Stealth in Integrated Systems Design, including jet-engine inlets and exhausts
Vectoring and safety in air, sea and land jet systems

Article formats
The journal welcomes scholarly research papers, invited review articles, and short communications

Volume 6 Issue 3-4

Issue of International Journal of Turbo & Jet-Engines

CONTENTS

Measurements of Thermal Radiation in Pressurized Turbulent Flames

Atomization Study in Jet Propulsion Lab. BIAA L A Survey Report

Studies on Aerated-Liquid Atomization

Application of the Vortex Cloud Method to Cascades

Prediction of Turbulence Generated Random Vibrational Response of Turbomachinery Blading

Optimization of the Arrangement of the Front and Rear Blade Rows of a Tandem Blade Cascade

Influence of Gas-Injector Geometry on Atomization Performance of Aerated-Liquid Nozzles

Holographic Interferometry for Flow Visualization Studies in High Speed Fans

Drop Size Measurement in Heated Air Flow and Experimental Study on the Interdependence of Spray Characteristics and Evaporation

Three-Dimensional Fluid Flow Phenomena in the Blade End Wall Corner Region

On the Choice of Centrifugal Impellers Semi-Open or Closed

Investigation and Experiment on a Short Dump-Diffuser of the Combustor

35MWIM5000 in Cogeneration Plant

CFD for Engine-Airframe Integration