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Title:Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surface (NACA Wartime Report L5C13)
Item ID:EC00-153401
Publisher:NACA/National Advisory Committee for Aeronautics, 1945
NACA/National Advisory Committee for Aeronautics, 1945, Softcover, Book Condition: Good

A couple library stamps and pencil notes on covers. Stapled edge, light wear, yellowing to the covers and pages but a good solid booklet overall. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 153401.
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