Frontmatter

Home Frontmatter

Article Publicly Available

Published/Copyright: March 4, 2017

Published by

Become an author with De Gruyter Brill

Author Information

"Frontmatter" International Journal of Turbo & Jet-Engines, vol. 34, no. 1, 2017, pp. i-iii. https://doi.org/10.1515/tjj-2017-frontmatter1

(2017). Frontmatter. International Journal of Turbo & Jet-Engines, 34(1), i-iii. https://doi.org/10.1515/tjj-2017-frontmatter1

(2017) Frontmatter. International Journal of Turbo & Jet-Engines, Vol. 34 (Issue 1), pp. i-iii. https://doi.org/10.1515/tjj-2017-frontmatter1

"Frontmatter" International Journal of Turbo & Jet-Engines 34, no. 1 (2017): i-iii. https://doi.org/10.1515/tjj-2017-frontmatter1

Frontmatter. International Journal of Turbo & Jet-Engines. 2017;34(1): i-iii. https://doi.org/10.1515/tjj-2017-frontmatter1

Copied to clipboard

Published Online: 2017-3-4

Published in Print: 2017-3-3

Articles in the same Issue

Frontmatter
Influence of Structural Parameters on the Performance of Vortex Valve Variable-Thrust Solid Rocket Motor
Numerical Studies on the Performance of Scramjet Combustor with Alternating Wedge-Shaped Strut Injector
Investigation of HP Turbine Blade Failure in a Military Turbofan Engine
Nozzle Admittance and Damping Analysis Using the LEE Method
Software Development for EECU Platform of Turbofan Engine
Numerical Study of the Propulsive Performance of the Hollow Rotating Detonation Engine with a Laval Nozzle
Analysis of Compressor Surge in a Military Turbojet Engine: A Case Study
The Combined Effects of Surface Roughness with Upstream Wakes on the Boundary Layer Development of an Ultra-High-Lift LPT Blade
Numerical Investigation of a Model Scramjet Combustor Using DDES
Flow Field Measurement in Multi-stage Axial Compressor Stator by Using Multi-hole Pneumatic Probes
Effect of Air Pressure and Gutter Angle on Flame Stability and DeZubay Number for Methane-Air Combustion
Control of Subsonic and Sonic Jets with Limiting Tabs

Search journal Search the content of this journal

Frontmatter
Influence of Structural Parameters on the Performance of Vortex Valve Variable-Thrust Solid Rocket Motor
Numerical Studies on the Performance of Scramjet Combustor with Alternating Wedge-Shaped Strut Injector
Investigation of HP Turbine Blade Failure in a Military Turbofan Engine
Nozzle Admittance and Damping Analysis Using the LEE Method
Software Development for EECU Platform of Turbofan Engine
Numerical Study of the Propulsive Performance of the Hollow Rotating Detonation Engine with a Laval Nozzle
Analysis of Compressor Surge in a Military Turbojet Engine: A Case Study
The Combined Effects of Surface Roughness with Upstream Wakes on the Boundary Layer Development of an Ultra-High-Lift LPT Blade
Numerical Investigation of a Model Scramjet Combustor Using DDES
Flow Field Measurement in Multi-stage Axial Compressor Stator by Using Multi-hole Pneumatic Probes
Effect of Air Pressure and Gutter Angle on Flame Stability and DeZubay Number for Methane-Air Combustion
Control of Subsonic and Sonic Jets with Limiting Tabs