Curtiss H: Difference between revisions
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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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Revision as of 14:43, 14 June 2022
The Curtiss H was a 40 hp (30 kW) water-cooled 4-cylinder in-line aero-engine.[1]
References
- ^ Angle, Glenn D. (1921). Airplane Engine Encyclopedia. Dayton, Ohio: THE OTTERBEIN PRESS.
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