Аеродинамічні дослідження інших тіл круглого поперечного перерізу, тіл обертання/Аэродинамические исследования прочих тел круглого поперечного сечения, тел вращения/Other bodies of round cross section. Rotation bodies
Документи:
- Аэродинамическая компенсация некоторых установок на самолете [Текст] / Я.М. Серебрийский. — М. : Изд-е ЦАГИ, 1936. — 19 с.
- Исследование теплообмена при струйном обтекании круглого цилиндра [Текст] : автореф. дис. ... канд. техн. наук / Куйбышев. авиац. ин-т. — Куйбышев, 1962. — 15 с.
- Краевая задача аэрогидродинамики проектирования осесимметричного тела с выдувом струи [Текст] / Н.Б. Ильинский, С.А. Соловьев // Известия вузов. Авиационная техника. — 2010. — С. 44-48.
- Метод расчета местных параметров несжимаемого потока около тел вращения [Текст] / А.И. Пастухов, В.Н. Кошевой, А.Д. Дерябин // Самолетостроение. Техника воздушного флота : респ. межведомств. науч. - техн. сб. / М-во высш. и сред. спец. образования УССР, Харьк. авиац. ин-т им. Н. Е. Жуковского. — Х. : Вища школа, 1988. — С. 5-9.
- О вращательном движении артиллерийского снаряда при немалых углах нутации [Текст] : автореф. дис. ... канд. физ.-мат. наук / ЛГУ им. А.А.Жданова. — Л., 1952. — 7 с.
- Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing Parameters [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 20 p.
- Analytic Study of Inducted Pressure on Long Bodies of Revolution with Varying Nose Bluntness at Hypersonic Speeds [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 18 p.
- An Investigation of the Effects of Heat Transfer on Boundry - Layer Transition on a Parabolic Body of Revolution (NACA RM - 10) at a Mach Number of 1.61 [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 11 p.
- A Theoretical Study of the Angular Motions of Spinning Bodies in Space [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 12 p.
- A Theoretical Study of the Torques Induced by a Magnetic Field on Rotating Cylinders and Spinning Thin-Wall Cones, Cone Frustums, and General Body of Revolution [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 15 p.
- A Unified Two - Dimentional Approach to the Calculation of Three - Dimentional Hypersonic Flows, With Application to Bodies of Revolution [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 27 p.
- Collection of Zero-Lift Drag Data on Bodies of Revolution From Free-Flight Investigations [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 188 p.
- Minimum - Drag Ducted and Pointed Bodies of Revolution Based on Linearized Supersonic Theory [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 9 p.
- On Boattail Bodies of Revolution Having Minimum Wave Drag [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 9 p.
- Slender-Body Theory Based on Approximate Solution of the Transonic Flow Equation [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 54 p.
- The Drag Coefficient of Parabolic Bodies of Revolution Operating at Zero Cavitation Number and Zero Angle of Yaw [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 18 p.
- Use of an Inertia Sphere to Damp the Angular Motions of Spinning Space Vehicles [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 12 p.
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