Publisher:National advisory Committee for aeronautics (NaCa), Washington, 1943
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 Charts for the Determination of wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal Speed; The Influence of Vertical Tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin Engine Airplane Model with One Engine Inoperative; Determination of the Stability and Control Characteristics of a Straight Wing, Tailless Fighter Airplane Model in the Langley Free Flight Tunnel; Charts for the Minimum Weight Design of 24S-T Aluminum Alloy Flat Compression Panels with Longitudinal Z-Section Stiffeners; more. 1942-1945. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 143093.