National Advisory Committee for Aeronautics (NACA) Wartime Report L391-L410

Various

Published by National advisory Committee for aeronautics (NaCa), Washington, 1943

About this Item

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 Characteristics of Beveled Trailing Edge Elevators on a Typical Pursuit Fuselage at Attitudes Simulating Normal Flight and Spin Conditions; Determination of the Damping Moment in Yawing for Tapered Wings with Partial Span Flaps; Calibrations of Pivot Static Tubes at High Speeds; Flight Tests of an All Movable Vertical Tail on the Fairchild XR2K-1 Airplane; The Strength and Stiffness of Shear Webs with and without Lightning Holes; Some Effects of Reynolds and Mach Numbers on the Lift of an NACA 0012 Rectangular Wing in the naca 19 Foot Pressure Tunnel; Wind Tunnel Investigation of Wing Ducts on a Single Engine Pursuit Airplane; more. 1942-1945. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 143096. This book is extra heavy, and may involve extra shipping charges to some countries. Seller Inventory # 143096

Bibliographic Details

Title: National Advisory Committee for Aeronautics ...

Publisher: National advisory Committee for aeronautics (NaCa), Washington

Publication Date: 1943

Binding: Hardcover

Condition: Good

Dust Jacket Condition: No Dust Jacket