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 The Influence of Bulkhead Spacing on Bending Stresses Due to Torsion; Flight Measurements of Compressibility Effects on a Three Blade Twin Clark Y PRopeller Operating at Constant Advance Diameter Ratio and Blade Angle; Wind Tunnel Investigation of a Full Span Retractable Flap in Combination with Full Span Plain and INternally Balanced Ailerons on a Tapered Wing; Wind Tunnel Investigation of Control Surface Characteristics XII-Various Cover Plate Alinements on the NACA 0015 Airfoil with a 30 Percent Chord Flap and Large Sealed internal Balance; Wind Tunnel Investigation of Shielded Horn Balances and Tabs on a 0.7 Scale Model of XF6F Vertical Tail Surface; more. 1943-1946. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 139044.