Results 341 to 350 of about 1,220,175 (393)

Computing machines in aircraft engineering [PDF]

open access: possiblePapers and discussions presented at the Dec. 10-12, 1951, joint AIEE-IRE computer conference: Review of electronic digital computers on - AIEE-IRE '51, 1951
A critical evaluation of computing machinery is given from the viewpoint of the aeronautical engineer. The machines' limitations are presented together with suggestions to make them more useful in the aircraft industry.
openaire   +3 more sources

Aircraft engine remaining useful life estimation via a double attention-based data-driven architecture

Reliability Engineering & System Safety, 2022
Lu Liu, Xiao-yong Song, Zhetao Zhou
semanticscholar   +1 more source

Alloy design for aircraft engines

Nature Materials, 2016
Metallic materials are fundamental to advanced aircraft engines. While perceived as mature, emerging computational, experimental and processing innovations are expanding the scope for discovery and implementation of new metallic materials for future generations of advanced propulsion systems.
openaire   +3 more sources

Demonstration of a Regulatory Method for Aircraft Engine Nonvolatile PM Emissions Measurements with Conventional and Isoparaffinic Kerosene fuels

, 2016
The aviation industry is exploring the economic viability and environmental sustainability of the use of alternative fuels to power aircraft main engines and auxiliary power units.
P. Lobo   +7 more
semanticscholar   +1 more source

Fuels for Aircraft Engines

Journal of the Royal Aeronautical Society, 1932
There has been a great advancement in recent years in the technique and production of suitable fuels for both aircraft and automobile engines and the author hopes that a few notes on the fuel problem with particular reference to aircraft work may be of help to those engaged on aero engine design and operation.In the author's opinion it is somewhat ...
openaire   +2 more sources

Exergoeconomic analysis of an aircraft turbofan engine

International Journal of Exergy, 2009
This study deals with an exergoeconomic analysis of an aircraft turbofan engine utilising the kerosene as fuel. A new parameter is developed to define the thrust cost rate. The cost of exergy destruction, the relative cost difference and the exergoeconomic factor are investigated.
Karakoc, T. Hikmet   +2 more
openaire   +4 more sources

Aircraft Engine Installation [PDF]

open access: possibleAircraft Engineering and Aerospace Technology, 1930
THE subject of aircraft engine installation has not received as much attention during the past as it should have done, particularly from an engineering and service standpoint. Many of the failures of power plants in the air have not been caused by engine failure, but by engine installation.
openaire   +2 more sources

Heat recovery from aircraft engines

Collection of Technical Papers. 35th Intersociety Energy Conversion Engineering Conference and Exhibit (IECEC) (Cat. No.00CH37022), 2000
The paper deals with the problem of heat recovery from aircraft engines, with specific reference to jet engines and turbo propeller engines. In actual propulsion systems, the trend for cycle maximum temperatures is for very high values, with a consequent increasing of discharge temperature, due account also given to operative modalities of the ...
ANDRIANI, ROBERTO   +3 more
openaire   +3 more sources

Multi-disciplinary optimisation approach for a light turboprop aircraft-engine integration and improvement

, 2016
Purpose The purpose of this paper is to present application of multidisciplinary design optimisation (MDO) in redesign of a small composite aircraft. The redesign process was integration of the turboprop engine in a small composite aircraft. The
A. Iwaniuk, W. Wiśniowski, J. Zóltak
semanticscholar   +1 more source

The Lubrication of Aircraft Engines

The Journal of the Royal Aeronautical Society, 1929
Mr. Foord: It has been truly said that “lubrication is the heart of an engine,” and I think this saying applies in the strongest possible sense to aircraft engines.The reasons for this are manifold and one has only to consider the overall thermal efficiency, the low weight/power ratio and consequent minimum scantlings and bearing surfaces, and the high
openaire   +2 more sources

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