Results 111 to 120 of about 21,160 (284)
Preliminary Evaluation of a Turbine/Rotary Combustion Compound Engine for a Subsonic Transport [PDF]
The fuel consumption of a modern compound engine with that of an advanced high pressure ratio turbofan was compared. The compound engine was derived from a turbofan engine by replacing the combustor with a rotary combustion (RC) engine. A number of boost
Civinskas, K. C., Kraft, G. A.
core +1 more source
Case Studies in Thermal EngineeringIt is widely agreed that the infrared stealth should be considered in the preliminary design phase of turbofan engine so as to decrease the infrared radiation of engine exhaust system.
Feng Wang +5 more
doaj +1 more source
On Intercooled Turbofan Engines [PDF]
, 2013 Kyprianidis, Konstantinos +2 more
openaire +3 more sources
Turboprop cargo aircraft systems study [PDF]
The effects of using advanced turboprop propulsion systems to reduce the fuel consumption and direct operating costs of cargo aircraft were studied, and the impact of these systems on aircraft noise and noise prints around a terminal area was determined.
Hewell, J. G., Jr. +5 more
core +1 more source
A remote augmentor lift system with a turbine bypass engine [PDF]
Two supersonic vertical takeoff or landing (VTOL) aircraft engine types, a conventional medium bypass ratio turbofan, and a turbine bypass turbojet were studied. The aircraft assumed was a clipped delta wing with canard configuration.
Fishbach, L. H., Franciscus, L. C.
core +1 more source
, 2014 The aim pursued by this project is to show the design of a complete turbofan. Because this design process is very complex and large groups of engineers for their development typically need the scope thereof in a final project is very limited. However, attempts to give an overview of what this design process and show the way forward from the work done ...
openaire +2 more sources
Performance assessment of the ducted propfan of the turbofan engine with ultra-high bypass ratio
, 2021 Олеся Валеріївна Денисюк
openalex +1 more source
NASA Quiet Clean General Aviation Turbofan (QCGAT) program status [PDF]
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small turbine engines and develop new technology where required is determined.
Bresnahan, D. L., Sievers, G. K.
core +1 more source
Effects of Tip Injection on a Turbofan Engine with Non-Invasive High-Speed Actuators [PDF]
Yannik Schäfer +3 more
openalex +1 more source
NASA/GE quiet engine C acoustic test results [PDF]
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The engine was built as a part of the Quiet Engine Program.
Kazin, S. B., Pass, J. E.
core +1 more source