Curtiss H: Difference between revisions
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{{Short description|Curtiss engine}} |
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The '''Curtiss H''' was a {{cvt|40|hp}} water-cooled 4-cylinder in-line aero-engine.<ref name="Angle">{{cite book |last1=Angle |first1=Glenn D. |title=Airplane Engine Encyclopedia |url=https://archive.org/details/airplaneenginee00anglgoog |date=1921|publisher=THE OTTERBEIN PRESS|location=Dayton, Ohio|pages=}}</ref> |
The '''Curtiss H''' was a {{cvt|40|hp}} [[water-cooled]] 4-cylinder in-line [[aero-engine]].<ref name="Angle">{{cite book |last1=Angle |first1=Glenn D. |title=Airplane Engine Encyclopedia |url=https://archive.org/details/airplaneenginee00anglgoog |date=1921|publisher=THE OTTERBEIN PRESS|location=Dayton, Ohio|pages=}}</ref> |
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==See also== |
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*[[Curtiss A-2]] |
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*[[Curtiss Aeroplane and Motor Company|Curtiss Aeroplane and Motor Company]] |
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==References== |
==References== |
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{{reflist}} |
{{reflist}} |
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[[Category: |
[[Category:Curtiss aircraft engines]] |
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Revision as of 22:29, 4 April 2024
The Curtiss H was a 40 hp (30 kW) water-cooled 4-cylinder in-line aero-engine.[1]
See also
References
- ^ Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio: THE OTTERBEIN PRESS.
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