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Numerical Tables for determination of the aerodynamic coefficients ca (lift coefficient), cw (drag coefficient) and the distance of center of pressure H/D (referred to caliber D)., 1941-01-15

 File — Box: 2, Folder: 14/17

Dates

  • Creation: 1941-01-15

Extent

From the Collection: 100 Linear feet

Language of Materials

From the Collection: German

General

German Translation: Bericht über Flugmechanik (Zahlentafeln zur Bestimmung der aerodynamischen Beiwerte ca, cw, und des Druckpunktabstandes H/D.)

Author/Editor: N/A

Repository Details

Part of the The University of Alabama in Huntsville Archives & Special Collections Repository

Contact:
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523