Results 111 to 120 of about 7,514 (171)
Recent Advances in Limiting Fatigue Damage Accumulation Induced by Self-Heating in Polymer-Matrix Composites. [PDF]
Amraei J, Katunin A.
europepmc +1 more source
Innovative Design and Fast Iterative Manufacturing of Micro-Turbojet Engines at Low Cost
The turbojet is the foundation of the gas turbine engine, which combines knowledge of fluid dynamics, thermodynamics, heat transfer, mechanical design, manufacturing, and jet propulsion. This paper describes in detail the inspiration source, design process, fluid dynamics analysis, manufacturing steps, ignition test method and test process of small jet
Yiding Zhang, Yitong Zhang
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A Thermodynamic Study of the Turbojet Engine
Charts are presented for computing thrust, fuel consumption, and other performance values of a turbojet engine for any given set of operating conditions and component efficiencies.
Karp, Irvin M, Pinkel, Benjamin
core
Influence of Boric Oxide Deposition on Turbojet-engine Operation
Influence of boric oxide deposition on turbojet engine ...
Burley, Richard R +5 more
core
Turbojet-engine Starting and Acceleration
From considerations of safety and reliability in performance of gas-turbine aircraft, it is clear that engine starting and acceleration are of utmost importance.
Straight, D. M., Mc Cafferty, R. J.
core
Blade design and thrust performance for a miniature turbojet engine
[[abstract]]A miniature turbojet engine was developed for the Unmanned Aerial Vehicle (UAV) applications. The development calls for a small and low cost turbojet engine, which will deliver 50 lbf thrust.
Tsai, Bor-Jang;Chiang, Hsiao-Wei;Luo, Yu-Shan
core
Design of A New Type Thrust Measuring System for Micro-turbojet Engine [PDF]
Zhan Lv +4 more
openaire +1 more source
The conference on Turbojet-Engine Thrust-Augmentation Research was organized by the NACA to present in summarized form the results of the latest experimental and analytical investigations conducted at the Lewis Flight Propulsion Laboratory on methods of ...
core
An analysis of turbojet-engine-inlet matching
A method of presenting turbojet-engine air-flow requirements and inlet-system air-flow capacities in identical though independent parametric terms is developed.
Wyatt, Demarquis
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Evaluation of methods for characterizing the fine particulate matter emissions from aircraft and other diffusion flame combustion aerosol sources. [PDF]
Giannelli R +22 more
europepmc +1 more source

