National Advisory Committee for Aeronautics (NACA) Wartime Report L51-L75

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 Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot Span Fighter Type Wing of NACA 230 Series Airfoil Sections; Lifting Surface Theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces; Wind Tunnel Investigation of a Rectangular NACA 2212 Airfoil with semispan Ailerons and with Nonperforated Balanced Double Split Flaps for use as Aerodynamic Brakes; Wind Tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail surface; An Automatically Variable Control Linkage and its Effect on the Lateral Control Characteristics of a High Speed Fighter Airplane; Airspeed Fluctuations as a Measure of Atmospheric Turbulence; more. 1943-1946. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 139038. This book is extra heavy, and may involve extra shipping charges to some countries. Seller Inventory # 139038

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