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)
Author:Hollingworth, Thomas A.
Publisher:NACA/National Advisory Committee for Aeronautics, 1945
Binding:Softcover
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.