Physics, asked by Anonymous, 3 months ago

Which of the following statement(s) is/are true with regards to Kutta condition for flow past airfoils?





(A) It is utilized to determine the circulation on an airfoil.

(B) It is applicable only to airfoils with sharp trailing edge.

(C) The trailing edge of an airfoil is a stagnation point.

(D) The flow leaves the trailing edge smoothly.​

Answers

Answered by HannuBro
25

Answer:

The caste system in India is the paradigmatic ethnographic example of caste. It has origins in ancient India, and was transformed by various ruling elites in medieval, early-modern, and modern India, especially the Mughal Empire and the British Raj.[1][2][3][4] It is today the basis of affirmative action programmes in India.[5] The caste system consists of two different concepts, varna and jati, which may be regarded as different levels of analysis of this system.

Answered by XxUNWANTEDSOULxX
0

Answer:

The Kutta condition is a principle in steady-flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist Martin Kutta.

The Kutta condition is a principle in steady-flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist Martin Kutta.Kuethe and Schetzer state the Kutta condition as follows:[1]:§ 4.11

The Kutta condition is a principle in steady-flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist Martin Kutta.Kuethe and Schetzer state the Kutta condition as follows:[1]:§ 4.11A body with a sharp trailing edge which is moving through a fluid will create about itself a circulation of sufficient strength to hold the rear stagnation point at the trailing edge.

The Kutta condition is a principle in steady-flow fluid dynamics, especially aerodynamics, that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist Martin Kutta.Kuethe and Schetzer state the Kutta condition as follows:[1]:§ 4.11A body with a sharp trailing edge which is moving through a fluid will create about itself a circulation of sufficient strength to hold the rear stagnation point at the trailing edge.In fluid flow around a body with a sharp corner, the Kutta condition refers to the flow pattern in which fluid approaches the corner from both directions, meets at the corner, and then flows away from the body. None of the fluid flows around the sharp corner.

Similar questions