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Acceleration Performance of Helicopter Engines

descriptionPublicationkeyboard_double_arrow_right Article 01 Apr 1987 English Publisher:ASME InternationalJournal:Journal of Engineering for Gas Turbines and Power, volume 109, pages 127-131 (issn: 0742-4795, eissn: 1528-8919, Copyright policy )
Authors: M. R. Maltby;

doi: 10.1115/1.3240014

Acceleration Performance of Helicopter Engines

Abstract

The desirability of good acceleration behavior from helicopter gas turbine engines is discussed in the context of the increasing demand for helicopter maneuverability and safety. Features which result in improved engine handling qualities are discussed and reference is made to some analytical techniques which may be employed to assist in obtaining the best results.

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
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