Advanced General Aviation Turbine Engine (GATE) concepts [PDF]
Concepts are discussed that project turbine engine cost savings through use of geometrically constrained components designed for low rotational speeds and low stress to permit manufacturing economies.
Lays, E. J., Murray, G. L.
core +1 more source
Helicopter Turboshaft Engine Emission Estimation Based on Standard Flight Profile [PDF]
Challenges to national defence in contemporary geopolitical situation, 2020 József TÓTH +2 more
openaire +1 more source
Automated Power Assessment for Helicopter Turboshaft Engines [PDF]
An accurate indication of available power is required for helicopter mission planning purposes. Available power is currently estimated on U.S. Army Blackhawk helicopters by performing a Maximum Power Check (MPC), a manual procedure performed by ...
Litt, Jonathan S., Simon, Donald L.
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Maintenance and inspection as risk factors in helicopter accidents: Analysis and recommendations. [PDF]
PLoS One, 2019 Saleh JH +3 more
europepmc +1 more source
A review of NASA's propulsion programs for aviation [PDF]
A review of five NASA engine-oriented propulsion programs of major importance to civil aviation are presented and discussed. Included are programs directed at exploring propulsion system concepts for (1) energy conservation subsonic aircraft (improved ...
Johnson, H. W. +2 more
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Propulsion System Models for Rotorcraft Conceptual Design [PDF]
The conceptual design code NDARC (NASA Design and Analysis of Rotorcraft) was initially implemented to model conventional rotorcraft propulsion systems, consisting of turboshaft engines burning jet fuel, connected to one or more rotors through a ...
Johnson, Wayne
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Fuel conservation merits of advanced turboprop transport aircraft [PDF]
The advantages of a propfan powered aircraft for the commercial air transportation system were assessed by the comparison with an equivalent turbofan transport.
Revell, J. D., Tullis, R. H.
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Multipoint Design and Optimization of a Turboshaft Engine for a Tiltwing Turboelectric Vertical Takeoff Landing Air Taxi [PDF]
This paper describes the design of a turboshaft engine for a tiltwing air taxi application. In this case, the tiltwing air taxi is intended to fly a 400 nm mission with up to fifteen passengers.
Chapman, Jeffryes W.
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Investigation on rub-impact response characteristics of gas generator rotor system under external excitation. [PDF]
Sci RepZhang H, Liu T, Zhao H, Wang Q.
europepmc +1 more source
Effects of helicopter transport on red blood cell components. [PDF]
Blood Transfus, 2012 Otani T +7 more
europepmc +1 more source