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Title:National Advisory Committee for Aeronautics (NACA) Wartime Report L294-L312
Item ID:EC00-143097
Publisher:National advisory Committee for aeronautics (NaCa), Washington, 1943
Dust Jacket:No
National advisory Committee for aeronautics (NaCa), 1943, Hardcover, Book Condition: Good, Dust Jacket Condition: No

Bound in one volume. Ex-library with reference marks, rebound; some wear to the covers, lightly discolored pages; a sound binding; very good otherwise. Includes A Study of the Tightness and Flushness of Machine Countersunk Rivets for Aircraft; Tapered Wings, Tip Stalling and Preliminary Results from Tests of the Stall Control Flap; Wind Tunnel Tests of Air inlet and Outlet Openings on a Streamline Body; A Theoretical Analysis of the Effect of Aileron Inertia and Hinge Moment on the Maximum Rolling Acceleration of Airplanes in Abrupt Aileron Rolls; The Effects of Angle of Dead Rise and Angle of Afterbody Keel on the Resistance of a Model of a Flying Boat Hull; Theory of Self Excited Mechanical Oscillations of Hinged Rotor Blades; Theory of Mechanical Oscillations of Rotors with Two Hinged Blades; more. 1942-1945. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 143097.
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