Matches in SemOpenAlex for { <https://semopenalex.org/work/W589555387> ?p ?o ?g. }
Showing items 1 to 77 of
77
with 100 items per page.
- W589555387 endingPage "601" @default.
- W589555387 startingPage "551" @default.
- W589555387 abstract "The decrease in the power output of aero-engines due to altitude has been already computed by several authorities. Most of them proceeded with the law of Welter that the quantity of heat liberated by the combustion of gasoline sucked into an engine cylinder is proportional to the weight of oxygen carried in with the gasoline. In this paper, the same problem is treated of, though the final result is not much difference, a little more theoretically from the thermodynamical point of view. Firstly, the formula for the mean effective pressure is deduced in terms of the pressure p and absolute temperature T of the fresh charge, the compression ratio ρ, the ratio γ of specific heats of the working fluid and the temperature rise ΔT due to the internal combustion. The first two factors p and T depend directly upon the conditions of the surrounding atmospheric air and the other two γ and ΔT upon the chemical compositions of gasoline and the ratio of air to gasoline in the fuel mixture as well as the ratio of compression. All of these factors are then computed theoretically, the results of which are applicable not only to gasoline engines but also to other internal combustion engines. The retaining of the horse power of aero-engines at high altitudes can be effected by two different systems-namely, by supercharging or increasing the compression ratio. The author's formulae may be used for the calculation of the latter system, which is of more interest in commercial service as it has an advantage for increasing fuel economy rather than power output. The author's own device for increasing the compression-expansion ratio is also described. So far the richness of the fuel mixture has been taken as constant at all altitudes. The effect of the variation of the richness is finally considered. In connection with this, the theory of the altimetric corrector for the carburation is treated of ; it must be, however, modified by the results of many experimental researches." @default.
- W589555387 created "2016-06-24" @default.
- W589555387 creator A5049582015 @default.
- W589555387 date "1925-01-01" @default.
- W589555387 modified "2023-10-16" @default.
- W589555387 title "EFFECT OF ALTITUDES ON THE POWER OF AERO-ENGINES" @default.
- W589555387 doi "https://doi.org/10.1299/jsmemagazine.28.101_551" @default.
- W589555387 hasPublicationYear "1925" @default.
- W589555387 type Work @default.
- W589555387 sameAs 589555387 @default.
- W589555387 citedByCount "0" @default.
- W589555387 crossrefType "journal-article" @default.
- W589555387 hasAuthorship W589555387A5049582015 @default.
- W589555387 hasBestOaLocation W5895553871 @default.
- W589555387 hasConcept C103697071 @default.
- W589555387 hasConcept C105923489 @default.
- W589555387 hasConcept C121332964 @default.
- W589555387 hasConcept C127413603 @default.
- W589555387 hasConcept C163258240 @default.
- W589555387 hasConcept C171146098 @default.
- W589555387 hasConcept C178790620 @default.
- W589555387 hasConcept C180016635 @default.
- W589555387 hasConcept C185592680 @default.
- W589555387 hasConcept C203311528 @default.
- W589555387 hasConcept C2524010 @default.
- W589555387 hasConcept C25797200 @default.
- W589555387 hasConcept C2775956859 @default.
- W589555387 hasConcept C33923547 @default.
- W589555387 hasConcept C39432304 @default.
- W589555387 hasConcept C39573554 @default.
- W589555387 hasConcept C511840579 @default.
- W589555387 hasConcept C57879066 @default.
- W589555387 hasConcept C6350597 @default.
- W589555387 hasConcept C78519656 @default.
- W589555387 hasConcept C97355855 @default.
- W589555387 hasConceptScore W589555387C103697071 @default.
- W589555387 hasConceptScore W589555387C105923489 @default.
- W589555387 hasConceptScore W589555387C121332964 @default.
- W589555387 hasConceptScore W589555387C127413603 @default.
- W589555387 hasConceptScore W589555387C163258240 @default.
- W589555387 hasConceptScore W589555387C171146098 @default.
- W589555387 hasConceptScore W589555387C178790620 @default.
- W589555387 hasConceptScore W589555387C180016635 @default.
- W589555387 hasConceptScore W589555387C185592680 @default.
- W589555387 hasConceptScore W589555387C203311528 @default.
- W589555387 hasConceptScore W589555387C2524010 @default.
- W589555387 hasConceptScore W589555387C25797200 @default.
- W589555387 hasConceptScore W589555387C2775956859 @default.
- W589555387 hasConceptScore W589555387C33923547 @default.
- W589555387 hasConceptScore W589555387C39432304 @default.
- W589555387 hasConceptScore W589555387C39573554 @default.
- W589555387 hasConceptScore W589555387C511840579 @default.
- W589555387 hasConceptScore W589555387C57879066 @default.
- W589555387 hasConceptScore W589555387C6350597 @default.
- W589555387 hasConceptScore W589555387C78519656 @default.
- W589555387 hasConceptScore W589555387C97355855 @default.
- W589555387 hasIssue "101" @default.
- W589555387 hasLocation W5895553871 @default.
- W589555387 hasOpenAccess W589555387 @default.
- W589555387 hasPrimaryLocation W5895553871 @default.
- W589555387 hasRelatedWork W1968781481 @default.
- W589555387 hasRelatedWork W2246739862 @default.
- W589555387 hasRelatedWork W2353492595 @default.
- W589555387 hasRelatedWork W2359883166 @default.
- W589555387 hasRelatedWork W2587857966 @default.
- W589555387 hasRelatedWork W2767582649 @default.
- W589555387 hasRelatedWork W2957409320 @default.
- W589555387 hasRelatedWork W3132481526 @default.
- W589555387 hasRelatedWork W3154445003 @default.
- W589555387 hasRelatedWork W2531743562 @default.
- W589555387 hasVolume "28" @default.
- W589555387 isParatext "false" @default.
- W589555387 isRetracted "false" @default.
- W589555387 magId "589555387" @default.
- W589555387 workType "article" @default.