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標(biāo)題: Titlebook: Aerodynamics; Peiqing Liu Textbook 2022 Science Press 2022 Hydrostatics.Fluid Kinematics.Fluid Dynamics.Plane Potential Flow.Ideal Incompr [打印本頁]

作者: Truman    時間: 2025-3-21 20:08
書目名稱Aerodynamics影響因子(影響力)




書目名稱Aerodynamics影響因子(影響力)學(xué)科排名




書目名稱Aerodynamics網(wǎng)絡(luò)公開度




書目名稱Aerodynamics網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Aerodynamics被引頻次




書目名稱Aerodynamics被引頻次學(xué)科排名




書目名稱Aerodynamics年度引用




書目名稱Aerodynamics年度引用學(xué)科排名




書目名稱Aerodynamics讀者反饋




書目名稱Aerodynamics讀者反饋學(xué)科排名





作者: MURKY    時間: 2025-3-21 22:09

作者: 政府    時間: 2025-3-22 01:58
Fundamentals of Viscous Fluid Dynamicsion theorem (constitutive relationship), the derivation of viscous flow differential equations (Navier–Stokes equations), the basic properties of viscous fluid motion, laminar flow and the basic characteristics of turbulence, the principle of similarity and dimensional analysis, etc.
作者: 逗它小傻瓜    時間: 2025-3-22 06:03

作者: municipality    時間: 2025-3-22 09:18

作者: Outwit    時間: 2025-3-22 16:15
Aerodynamic Characteristics of Flow Over Low-Speed Airfoilsent history, airfoil aerodynamic coefficient, airfoil flow, and aerodynamic characteristics, determination of Kutta–Joukowski trailing-edge condition and circulation, generation mechanism of airfoil lift, development of airfoil near boundary layer, solution of steady incompressible potential flow ar
作者: 殺菌劑    時間: 2025-3-22 17:07

作者: itinerary    時間: 2025-3-22 21:38

作者: 惡臭    時間: 2025-3-23 02:36
Aerodynamic Characteristics of Subsonic Thin Airfoil and Wing derivation of the ideal steady compressible velocity potential function equation, the theory of small disturbance linearization, the theoretical solution of the two-dimensional subsonic streamline around the corrugated wall, the compressibility correction method, and its application (the Prandtl-Gl
作者: OVERT    時間: 2025-3-23 08:22

作者: MILL    時間: 2025-3-23 11:24

作者: Ataxia    時間: 2025-3-23 16:53
High Lift Devices and Their Aerodynamic Performancest device, the basic type of the high lift device, the support and driving mechanism of the high lift device, the aerodynamic principle of the high lift device, the aerodynamic noise of the high lift device, the wind tunnel experiment and calculation method of the high lift device, and the combined c
作者: Melatonin    時間: 2025-3-23 18:31
https://doi.org/10.1007/978-981-19-4586-1Hydrostatics; Fluid Kinematics; Fluid Dynamics; Plane Potential Flow; Ideal Incompressible Fluid; Viscous
作者: PAN    時間: 2025-3-23 22:58
Peiqing LiuFocuses on theoretical fundamentals while leading students through aeronautics applications.Strengthens the understanding of theoretical derivation to inspire innovation.Includes latest research advan
作者: CERE    時間: 2025-3-24 03:52

作者: audiologist    時間: 2025-3-24 10:02

作者: 斜谷    時間: 2025-3-24 14:02

作者: Monocle    時間: 2025-3-24 15:17

作者: 異教徒    時間: 2025-3-24 22:06

作者: 金哥占卜者    時間: 2025-3-25 01:52
https://doi.org/10.1007/978-3-642-57414-6This chapter mainly introduces the definition of aerodynamics, research objects and tasks.
作者: Collected    時間: 2025-3-25 03:41

作者: tympanometry    時間: 2025-3-25 08:41
https://doi.org/10.1007/978-3-642-57414-6This chapter mainly introduces the Lagrange method and Euler method to describe the fluid motion, the motion characteristics of fluid particles (streamline, trace, etc.), and the change rate of physical quantities of fluid particles (including velocity, acceleration, material derivative of physical quantities, etc.).
作者: 殺子女者    時間: 2025-3-25 14:28

作者: Tortuous    時間: 2025-3-25 16:06
Basic Properties of Fluids and HydrostaticsThis chapter mainly introduces the continuum assumption, the flow of fluid, the basic mechanical properties.
作者: avarice    時間: 2025-3-25 21:41
Foundation of Fluid Kinematics and DynamicsThis chapter mainly introduces the Lagrange method and Euler method to describe the fluid motion, the motion characteristics of fluid particles (streamline, trace, etc.), and the change rate of physical quantities of fluid particles (including velocity, acceleration, material derivative of physical quantities, etc.).
作者: Inflamed    時間: 2025-3-26 01:40

作者: 壟斷    時間: 2025-3-26 05:17
Controlling the Electoral Marketplaceion theorem (constitutive relationship), the derivation of viscous flow differential equations (Navier–Stokes equations), the basic properties of viscous fluid motion, laminar flow and the basic characteristics of turbulence, the principle of similarity and dimensional analysis, etc.
作者: 分離    時間: 2025-3-26 12:16

作者: 出汗    時間: 2025-3-26 14:12

作者: 低能兒    時間: 2025-3-26 18:50

作者: RENIN    時間: 2025-3-26 22:01

作者: OREX    時間: 2025-3-27 03:32

作者: 營養(yǎng)    時間: 2025-3-27 08:20

作者: 固定某物    時間: 2025-3-27 09:50
Controlling the World Bank and IMFic theory of thin airfoil and aerodynamic force characteristics, aerodynamic characteristics of an oblique wing with an infinite wingspan at supersonic flow, phenomena and aerodynamic characteristics of a thin wing at supersonic flow, lift characteristics of rectangular flat wing at supersonic flow,
作者: lethargy    時間: 2025-3-27 15:18
Controlling the World Bank and IMFic airfoil flow, transonic thin airfoil flow phenomenon and aerodynamic characteristics, transonic small perturbation potential flow equation and similarity rule, the influence of wing geometric parameters on transonic critical Mach number, and aerodynamic characteristics of supercritical airfoil fl
作者: pester    時間: 2025-3-27 19:16

作者: Cleave    時間: 2025-3-27 22:56
Fundamentals of Viscous Fluid Dynamicsion theorem (constitutive relationship), the derivation of viscous flow differential equations (Navier–Stokes equations), the basic properties of viscous fluid motion, laminar flow and the basic characteristics of turbulence, the principle of similarity and dimensional analysis, etc.
作者: 失誤    時間: 2025-3-28 06:00

作者: 高度表    時間: 2025-3-28 08:57

作者: Mediocre    時間: 2025-3-28 12:38
Aerodynamic Characteristics of Subsonic Thin Airfoil and Wing derivation of the ideal steady compressible velocity potential function equation, the theory of small disturbance linearization, the theoretical solution of the two-dimensional subsonic streamline around the corrugated wall, the compressibility correction method, and its application (the Prandtl-Glauert compressibility correction).
作者: 濕潤    時間: 2025-3-28 17:45
https://doi.org/10.1007/978-94-009-3275-3French physicist, Couette) and Fully developed laminar pipe flow (Poiseuille flow, French physiologist Poiseuille, 1799~1869), Stokes (Stokes, 1819–1903) solution for small Reynolds number spheres, etc. A large number of problems in practice can only be solved by approximate methods.
作者: 注意到    時間: 2025-3-28 20:57

作者: Middle-Ear    時間: 2025-3-29 02:56
Valuing the Froth on a Pint of Beer,surface theory of wing, low-speed aerodynamic characteristics of low aspect ratio wing, engineering estimation of low-speed aerodynamic characteristics of wing, and aerodynamic characteristics of the control surface.
作者: 漫不經(jīng)心    時間: 2025-3-29 05:54
Boundary Layer Theory and Its ApproximationFrench physicist, Couette) and Fully developed laminar pipe flow (Poiseuille flow, French physiologist Poiseuille, 1799~1869), Stokes (Stokes, 1819–1903) solution for small Reynolds number spheres, etc. A large number of problems in practice can only be solved by approximate methods.
作者: 偶像    時間: 2025-3-29 07:25

作者: 討好美人    時間: 2025-3-29 12:18
Aerodynamic Characteristics of Low Speed Wing Flowsurface theory of wing, low-speed aerodynamic characteristics of low aspect ratio wing, engineering estimation of low-speed aerodynamic characteristics of wing, and aerodynamic characteristics of the control surface.
作者: 我的巨大    時間: 2025-3-29 16:04

作者: MEAN    時間: 2025-3-29 21:22

作者: Ondines-curse    時間: 2025-3-30 01:33
Controlling the World Bank and IMFc flow, phenomena and aerodynamic characteristics of a thin wing at supersonic flow, lift characteristics of rectangular flat wing at supersonic flow, and characteristic line theory of supersonic flow.
作者: judicial    時間: 2025-3-30 06:19

作者: cravat    時間: 2025-3-30 09:42
https://doi.org/10.1007/978-3-658-06056-5t device, the aerodynamic noise of the high lift device, the wind tunnel experiment and calculation method of the high lift device, and the combined control technology of the trailing-edge hinge flap and the lower deflection of the spoiler.
作者: intuition    時間: 2025-3-30 16:21





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