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

Materials in design, I have assignments to due and I''m wondering if you co...

I have assignments to due and I''m wondering if you could do it for me

System dynamics , System Dynamics  Crucial to the development of a guid...

System Dynamics  Crucial to the development of a guidance system is an understanding of the dynamics of the system. In particular, it is necessary to understand how the acceler

Engineering Chemistry , How much heat in kJ is released when 4.1 grams of e...

How much heat in kJ is released when 4.1 grams of ethanol burns? C2H5OH(l) + 3 O2(g) ? 2 CO2(g) + 3 H2O(l), ?H = -1366.8 kJ/mol rxn

Resonance, explain amplitude resonance

explain amplitude resonance

Aviation legislation - Variant Aircraft, Variant Aircraft A variant air...

Variant Aircraft A variant aircraft is one that embodies certain design features which differ from one for which a Certificate of Airworthiness (C of A) has previously been iss

Finite element analysis, List the advantages disadvantages and applications...

List the advantages disadvantages and applications of FEM?

Coding system, What is the possible problem if there is more than one part ...

What is the possible problem if there is more than one part having the same code?

Finding depreciation and amoritizaton, EBITDA is 7.5 million, Net income is...

EBITDA is 7.5 million, Net income is 1.8, 2.0 million is interest expense, corporate tax is 40%. What is the Depreciation and amortization?.

Longitudinal trim, A trimmed flight condition is perhaps best thought of as...

A trimmed flight condition is perhaps best thought of as an equilibrium condition. The simplest trim condition is straight-and-level flight, in which the forces (weight, propulsive

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