Performance characteristics of a Junkers Jumo 211F engine supercharger with a DVL fully shrouded impeller and scroll diffuser /
J. Austin King and Harold Klein.

Description

Main Author

King, J. Austin.

Related Names

Klein, Harold.
Aircraft Engine Research Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, [1945]

Subjects

Charts, diagrams, etc.
Diffusers.
Impellers.
Junkers airplanes.
Airplanes > Airplanes / Motors > Airplanes / Motors / Performance.
Airplanes > Airplanes / Motors > Airplanes / Motors / Superchargers.

Summary

A German supercharger from a Junkers Jumo 211F engine was tested by the NACA. The supercharger differed from conventional American superchargers in that it had a fully shrouded impeller, which discharged through a very short vaneless diffuser into a scroll-collector case.

Note

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.
Originally issued as NACA as Advance Restricted Report E5B03 (February 1945).
NACA Wartime Report E-3.

Physical Description

10, [19] p. : ill. ; 27 cm.

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