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The Aerodynamic Effect of a Retractable Landing Gear (1933)

NASA Technical Reports Server (NTRS) · leaf 5

An illustration from The Aerodynamic Effect of a Retractable Landing Gear, 1933, leaf 5
Figure 2.-Lockheed Altair with landing gear extended and wheel wells open.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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