Зведений каталог бібліотек Харкова

• Класифікатори та каталоги
• Аеродинамічні дослідження окремих частин літальних апаратів

Крила. Обводи крил/Крылья. Обводы крыльев/Wings. Contours of the wings

Підтеми:

• Cтреловидне крило/Стреловидное крыло/Sweptwing
• Нестреловидне крило/Нестреловидное крыло/Nonsweptwing
• Прямокутне крило/Прямоугольное крыло/Rectangular wing

Документи:

• Calculation of the Lateral Control of Swept and Unswept Flexible Wings of Arbitrary Stiffness [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 19 p.
• Calculations on the Forces and Moments for an Oscillating Wing - Aileron Combination in Two - Dimentional Flow at Sonic Speed [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 16 p.
• Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form With Particular Reference to Delta Wings [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 20 p.
• Effect of Aspect Ratio on the Air Forces and Moments of Harmonically Oscillating Thin Rectangular Wings in Supersonic Potential Flow [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Gowernment Printing Office, 1951. — 17 p.
• Effects of Wing Position and Fuselage size on the Low - Speed Static and Rolling Stability Characteristics of a Delta - Wing Model [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 31 p.
• Elliptic Cones Alone and With Wings at Supersonic Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 24 p.
• Etude Methodique de L'aile Trapezoidale en Consideration du Decrochement [Текст] / A.D. Lajarte. — Paris : Ed. Blondel La Rougery, 1942. — 24 p.
• Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 27 p.
• Flexure-Torsion Flutter Derivatives for Semi-Rigid Wings [Текст] / Aeronautical Research Committee Reports and Memoranda. — London : His Majesty's Stationery Office, 1941. — 25 p.
• Formulars for the Supersonic Loading, Lift and Drag of Flat Swept - Back Wings with Leading Edges Behind the Mach Lines [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1951. — 40 p.
• Generalized Indication Forces on Deforming Rectangular Wings in Supersonic Flight [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 27 p.
• Investigation of Some Wake Vortex Characteristics of an Inclined Ogive-Cylinder Body at Mach Number 2 [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 19 p.
• Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 60 p.
• On the Application of Transonic Similarity Rules to Wings of Finite Span [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 21 p.
• On the Kernel Function of the Integral Equation Relating the Lift and Downwash Distributions of Oscilating Finite Wings in Subsonic Flow [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 16 p.
• Quasi - Cylindrical Theory of Wing - Body Interference at Supersonic Speeds and Comparison With Experiment [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 56 p.
• The Effect of Fuselage and Nacelles on Wing Bending Moment, Shear and Torsion [Текст] / Ministry Of Aircraft Production. — London : His Majesty's Stationery Office, 1943. — 18 p.
• The Effects on Dynamic Lateral Stability and Control of Large Artificial Variations in the Rotary Stability Derivatives [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 24 p.
• The Evaluation of Downwash at Large Spanwise Distances from a Vortex Lattice [Текст] / Ministry of Supply. — London : Her Majesty's Stationery Office, 1953. — 8 p.
• The Hydrodynamic Characteristics of Modified Rectangular Flat Plates Having Aspect Ratios of 1.00, 0.25, and 0.125 and Operating Near a Free Water Surface [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 50 p.
• Wind - tunnel Tests on the Prevention of Boundry - Layer Separation by Distributed Suction at the Rear of a Thick Aerofoil (NPL 153) [Текст] / Ministry of Supply. — London : Her Majesty's Stationery Office, 1953. — 7 p.

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