Cтреловидне крило/Стреловидное крыло/Sweptwing
Документи:
- Аэродинамические характеристики крыла обратной стреловидности, обтекаемого со скольжением. [Текст] / М.А. Фефелов // Прикладные задачи аэромеханики : темат. сб. науч. тр. / ХАИ им. Н.Е. Жуковского. — Х. : ХАИ, 1987. — С. 77-81.
- Аэродинамические характеристики модели буксируемого устройства со стреловидным крылом большого удлинения и оперением [Текст] : отчет о НИР (промежуточ.) : 101-38/79 / ХАИ им. Н.Е.Жуковского ; рук. Андренко Г.И. ; исполн.: Гамануха А.И. — Х., 1981. — 38 с.
- Исследование развития нестационарного отрыва потока на модели со стреловидным крылом [Текст] / И.В. Колин, В.Г. Марков, В.Л. Суханов та ін. // Известия РАН. Механика жидкости и газа. — М. : Наука, 2000. — С. 60-67.
- Исследование разрезного крыла с применением электрической аналогии [Текст] : автореф. дис. ... канд. техн. наук / Казан. авиац. ин-т. — Казань, 1958. — 16 с.
- Исследование суммарных и распределенных аэродинамических характеристик крыльев прямой и обратной стреловидности малого удлинения [Текст] : отчет о НИР (промежуточ.) : Г101-90/86 / ХАИ ; рук. Фефелов М.А. ; исполн.: Фефелов М.А. — Х., 1986. — 79 с.
- Прочность и устойчивость косоугольных свободно опертых пластинок [Текст] : автореф. дис. ... канд. техн. наук / МАИ им. С.Орджоникидзе. — М., 1953. — 10 с.
- Труды [Текст] / НКТП СССР; ГУАП. — М. : Изд. отд. ЦАГИ, 1935. — 18 с.
- A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch - up of a Swept - Wing Airplane in Maneuvering Flight at Transonic Speeds [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 12 p.
- A Method of Colution with Tabulated Results for the Attached Oblique Shock-Wave System for Surfaces at Various Angles of Attack, Sweep, and Dihedral in an Equilibrium Real Gas [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 141 p.
- An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 57 p.
- An Evaluation of Effects of Flexibility on Wing Strains in Rough Air for a Large Swept-Wing Airplane by Means of Experimentally Determined Frequency-Response Functions with an Assessment [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 33 p.
- Area-Suction Boundry-Layer Control as Applied to the Trailing-Edge Flaps of a 35 Swept-Wing Airplane [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 33 p.
- A Study of the Zero-Lift Drag-Rise Characteristics of Wing-Body Combinations Near the Speed of Sound [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 22 p.
- Blowing-Type Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 Swept-Wing Airpane [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 23 p.
- Calculated Responses of a Large Swepting Airplane to Continuous Turbulence with Flight-Test Comparisons [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 25 p.
- Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 25 p.
- Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Loading of Swept and Unswept Wings [Текст] : Report / National Advisory Committee For Aeronautics. — Washington : U.S. Government Printing Office, 1953. — 48 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.
- Summary and Analysis of Horizontal-Tail Contribution to Longitudinal Stability of Swept-Wing Airplanes at Low Speeds [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 87 p.
- The Dynamic - Response Characteristics of a 35 Swept - Wing Airplane as Determined from Flight Measurements [Текст] : Report / National Advisory Committee for Aeronautics. — Washington : U.S. Government Printing Office, 1955. — 25 p.
- The Effect of Endplates on Swept Wings [Текст] : Report / Ministry of Supply. — London : Her Majesty's Stationery Office, 1952. — 11 p.
- Wind-Tonnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Swept-Wing Airplane [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1956. — 24 p.
- Wind - Tunnel Investigation at Low Speed of the Effects of Chordwise Wing Fences and Horizontal - Tail Position on the Static Longitudinal Stability Characteristics of an Airplane Model Wing [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1954. — 29 p.
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