Aerodynamics-flow model diagram , Other Engineering

Assignment Help:

We will need to use several different flow models as we go along. It is crucial to understand the simplifications used to obtain these models because these limit the validity of the predictions.

We will use a model diagram to keep track of the simplifications and models. We will make a start at constructing this diagram now, and you will then keep it updated as we progress through the module.

 

Method

 

The diagram will initially have the following structure:

2304_areodynamics.png

Each arrow represents simplifications to derive the lower equations from the more general upper

equations.

 

(a) Read Anderson section 1.10 to obtain an idea of the types of flow that can be encountered

(b) By reading in Anderson, try to identify what simplifications have been used at each of the arrows above. For the Euler Equations, see sections 2.4-2.6, for Potential Flow look to section 3.7, and for the Boundary Layer equations look to sections 18.1 and 18.2. Note that the Navier-Stokes equations are given in the summary box of  chapter 2 (i.e. the "basic flow equations").

 

 

 


Related Discussions:- Aerodynamics-flow model diagram

Circuit Problem, Please solve this problem fully http://i39.tinypic.com/6...

Please solve this problem fully http://i39.tinypic.com/64h3kl.png

Numerical method, find the newton raphson iterative formula for a reciproca...

find the newton raphson iterative formula for a reciprocal of a number N and hence find the value of 1/23.correct to 5 place of decimal

Matlab, 2. Write a MATLAB program to perform discounted reward value iterat...

2. Write a MATLAB program to perform discounted reward value iteration. Show me the MATLAB code and also an output from your code for solving the problem provided in the data above

Engine drains, ENGINE DRAINS. There are two types of drains: • Con...

ENGINE DRAINS. There are two types of drains: • Controlled drains - the result of normal operation. • Uncontrolled drains - the result of abnormal operation. CONTROLLE

Damping coefficint of canatrd of aircraft, what will be the methodology to ...

what will be the methodology to calculate pitching moment damping coefficient of canrad of aircraft

Aeroengines - comparison with analytical solution, The figure below compare...

The figure below compares the discrete solution with the exact analytical solution The error is largest at the right boundary where it is equal to solution. The error is largest at

Weighted average cost of capital, 3. Earthway Corporation has target capit...

3. Earthway Corporation has target capital structure of 60 percent common stock, 5 percent preferred stock and 35 percent debt. Its cost of equity is 12.5 percent, the cost of pr

LAVOISIER LAPLACE''S LAW, GIVE EXPLANATION HOW THIS IS USEFUL IN APPLICATIO...

GIVE EXPLANATION HOW THIS IS USEFUL IN APPLICATION OF THERMODYNAMICS TOWARDS CHEMICAL PROCESS

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd