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- On the Design of Energy Efficient Aero Engines Some Recent Innovations
- Combustor Chambers - A.G
- Materials for Gas Turbines – an Overview
- Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT)
- Turbulent Combustion in Gas Turbine Engines
- New Technology Used in Gas Turbine Blade Materials
- Materials for Aircraft Engines
- Fundamentals of Gas Turbine Engines
- Scaling of Performance in Liquid Propellant Rocket Engine Combustion Devices
- Fundamentals of Gas Turbine Engines
- Aircraft Engine Operation and Malfunction
- Gas Turbine Reverse-Flow Combustor Research
- AE 1107C Turboshaft
- Design, Manufacturing and Rig Test of a Small Turbojet Engine Combustor with Airblast Atomizer
- One-Dimensional Analysis of Double Annular Combustor for Reducing Harmful Emissions
- Pdf Ger-3551
- TAPS II Public Final
- Analysis of the Effects of Methane Ingestion on Turboshaft Engines
- Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
- Gas-Fired Distributed Energy Resource Technology Characterizations
- 14 Transition to Turbopropeller Powered Airplanes
- Evaluation of Performance Properties of Two Combustor Turbofan Engine
- Airbreathing Propulsion for Defense of the Surface Fleet
- Scramjet Combustor Design - a Review Varsha Rani*, Ayush Passi Department of Aerospace Engineering, Amity Institute of Aerospace Engineering, Uttar Pradesh, India
- Rocket Combustor Experiments and Analyses
- Combustor Characteristics
- Supercritical Mixing and Combustion in Rocket Propulsion
- Key Technologies for 1700℃ Class Ultra High Temperature Gas Turbine
- Ramjet Combustion Chamber
- Large-Eddy Simulations of a Sub-Scale Liquid Rocket Combustor: Influence of Fuel Injection Temperature on Thermo-Acoustic Stability
- Research on Modeling of a Micro Variable-Pitch Turboprop Engine Based on Rig Test Data
- Airplane Flying Handbook (FAA-H-8083-3B) Glossary
- T55 TURBOSHAFT ENGINE Continuous Improvement of a Battlefield Proven Engine
- Design and Construction of a Simple Turbojet Engine
- SF-1600: a Next Generation High Efficiency Turboprop for Single- Engine Aircraft Design Team: Elliot Bicker # 531124 ______
- Modeling of a Sequential Two-Stage Combustor
- NASA and General Aviation. NASA SP-485. INSTITUTION National Aeronautics and Space Administration, Washington, DC
- Catalog of CHP Technologies, Full Report, September 2017
- ME925-Fundamentals of Gas Turbine Engines
- Numerical Investigation of Multi-Phase Trapped Vortex Combustor and Afterburner with Pulse Injection Using Jet-A Fuel
- Air Starting Systems for Marine Gas Turbine Engines
- Turbojets, Turbopropellers and Other Gas Turbines, (HTSUS 8411) and Parts Thereof
- Analysis of an After Burner in a Jet Engine
- The Talos Propulsion System
- Characterization of the Reacting Two-Phase Flow Inside a Research Ramjet Combustor
- Conventional Type Combustion 3.2.1.1-1 Introduction
- Introduction to a Single-Shaft Turboprop Engine
- Combustor Designs for Low Emissions
- A Methodology for Afterburner Evaluation
- And Jet-Fueled Turbofan Aero Engine
- ICAO Presentation
- 4.2.1-1 Introduction Cooling Design Analysis Ron S. Bunker