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- Improved Design of Large Wind Turbine Blade of Fibre Composites Based on Studies of Scale Effects (Phase 1) - Summary Report
- New Technology Used in Gas Turbine Blade Materials
- Materials for Aircraft Engines
- Rocket Engines: Turbomachinery
- CJ-3000 Turbofan Engine Design Proposal
- RS-25 Incredible Facts
- 4.3 Turbine Blade Aerodynamics Endwall Region Which Causes the Cross flow Here to Be Stronger
- Variable Pitch Approach for Performance Improving of Straight-Bladed VAWT at Rated Tip Speed Ratio
- Notice of Proposed Amendment 2015-22
- Federal Aviation Administration, DOT § 33.96
- Single Crystal Turbine Blade
- Multi Objective Design Optimization of Rocket Engine Turbopump Turbine
- Rotordynamic Analysis of Asymmetric Turbofan Rotor Due to Fan Blade-Loss Event with Contact-Impact Rub Loads Sunil Sinha
- Making Lighter Aircraft Engines with Titanium Aluminide Blades
- System Analysis of a Gas Generator Cycle Rocket Engine
- Propeller Design for Conceptual Turboprop Aircraft
- Federal Register/Vol. 77, No. 180/Monday, September 17, 2012
- Issue No. 1, Jan-Mar
- Coating Applications for Aviation Engines
- The Use of Platform Dampers to Reduce Turbine Blade Vibrations
- Key Technologies for 1700℃ Class Ultra High Temperature Gas Turbine
- Study of Materials Used in Gas Turbine Engine and Swirler in Combustion Chamber 1Prashant Singh, Kalpit P
- Engine and APU Failure Loads and Sustained Engine Windmilling
- FAA Advisory Circular AC 33-5: Turbine Engine Rotor Blade
- 93-Gt-222 a Review of the Full Capabilities of Blade Path
- TECHNICAL REPORT on Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards
- SF-1600: a Next Generation High Efficiency Turboprop for Single- Engine Aircraft Design Team: Elliot Bicker # 531124 ______
- Gas Turbine Engine Motoring System for Bowed Rotor Engine Starts
- Bleedless” and “Bleed Air” Gas Turbine Engines
- Design Procedure and Analysis of Turbine Rotor Fragment Hazard
- Mechanical Design of Turbojet Engines – an Introduction
- Wind Generator Innovative Blade Design: Variable Twist and Start-Up Control
- Recycling Wind Turbine Blade Composite Material As Aggregate in Concrete
- Thermo-Mechanical Modeling of a High Pressure Turbine Blade of an Airplane Gas Turbine Engine Mechanical Engineering
- ME925-Fundamentals of Gas Turbine Engines
- Design and Analysis of a High Speed, High Pressure Peroxide RP-1
- Air Starting Systems for Marine Gas Turbine Engines
- Hypersonic Airbreathing Propulsion
- Wind Turbine Blade Design
- Turbine Blade Temperature Field Prediction Using the Numerical Methods
- ME1230-Jet Turbine Engine Fundamentals
- Analysis of an Advanced Technology Subsonic Turbofan Incorporating Revolutionary Materials
- On the Fabrication of Metallic Single Crystal Turbine Blades with a Commentary on Repair Via Additive Manufacturing
- Analysis of a J69-T-25 Engine Turbine Blade Fracture Myounggu Park, Young-Ha Hwang, Yun-Seung Choi, Tae-Gu Kim
- United States Patent [191 [Ill Patent Number: 4,913,623 Schilling Et Al
- Materials for Advanced Rocket Engine Turbopump Turbine Blades W. T
- Feasible Concept of an Air-Driven Fan with a Tip Turbine for a High-Bypass Propulsion System
- 4.2.1-1 Introduction Cooling Design Analysis Ron S. Bunker