Results 281 to 290 of about 847,370 (336)
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HELICOPTER ENGINE FOREIGN OBJECT DAMAGE
2017<div class="section abstract"> <div class="htmlview paragraph">The purpose of this SAE Aerospace Information Report is to disseminate qualitative information regarding foreign object damage (FOD) to gas turbine engines used to power helicopters and to discuss methods of preventing FOD.
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Twin Engine Helicopter Power Requirements
2017<div class="section abstract"> <div class="htmlview paragraph">This SAE Aerospace Information Report (AIR) defines the power spectrum during normal and emergency operations of a twin engine helicopter and thereby postulates suitable power plant rating structures.
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A World Of Applications For Helicopter Electromagnetics To Environmental And Engineering Problems
12th EEGS Symposium on the Application of Geophysics to Engineering and Environmental Problems, 1999The variety of environmental and engineering applications for helicopter-borne electromagnetic surveys has increased in recent years. Helicopter EM surveys undertaken by Geoterrex-Dighem have been used for: l measuring soil conductivity near oil pipelines to assess corrosion risk, l estimating soil type and depth for pipeline planning, l mapping sand ...
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Rethinking the Paper Helicopter
The American Statistician, 2005Box's paper helicopter has been used to teach experimental design for more than a decade. It is simple, inexpensive, and provides real data for an involved, multifactor experiment. Unfortunately it can also further an all-too-common practice that Professor Box himself has repeatedly cautioned against, namely ignoring the fundamental science while ...
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THE RECIPROCATING ENGINE IN THE HELICOPTER
SAE Technical Paper Series, 1953J. J. SHIELDS, J. T. BOWLING
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An engine for tomorrow's small helicopters
20th Joint Propulsion Conference, 1984E. COHEN, D. JACOBY
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Some Aspects of Turboshaft Engine Installations in Multi-engined Helicopters
The Journal of the Royal Aeronautical Society, 1964In projecting future turboshaft engines for helicopter appUcations the engine designer is faced with the problem of selecting the size of engine to meet the likely size, configuration, performance and economic requirements of future helicopters. It is also desirable to meet as many different helicopter applications as possible with the same basic ...
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Review of thermoelectric generation for internal combustion engine waste heat recovery
Progress in Energy and Combustion Science, 2022Nicolae Vlad Burnete +2 more
exaly
The RTM322 engine in the S-70C helicopter
Aircraft Design, Systems and Operations Conference, 1988PAUL SCEARS, PETER SEWELL
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