dc.contributor.author |
Ali, Esra Abd Alhleem Hassan |
|
dc.date.accessioned |
2014-01-09T10:10:27Z |
|
dc.date.available |
2014-01-09T10:10:27Z |
|
dc.date.issued |
2010-01-01 |
|
dc.identifier.citation |
Ali,Esra Abd Alhleem Hassan.A STUDY SUBSONIC AND HYPERSONIC FLOW ON AN AIRFOIL/Esra Abd Alhleem Hassan Ali;Osman Mohamed El-Mekki.-Khartoum:Sudan University of Science and Technology,College of Science,2010.-41p. : ill. ; 28cm.-M.Sc. |
en_US |
dc.identifier.uri |
http://hdl.handle.net/123456789/3091 |
|
dc.description |
Thesis |
en_US |
dc.description.abstract |
First
in this research I study's about (subsonic
and hypersonic flows on an airfoil)which consists
of three Chapters; Chapter one by the title:
(Compressible
Potential
Flow)contains:
Introduction, Speed of sound, Irrotational flow,
:Linearized potential equation which includes
Applications, Perturbation potentials), Pressure )
coefficient of small perturbations, Relation for
subsonic compressible flow including (Airfoils (2-D
flow), Boundary conditions, Pressure coefficients),
.Critical Mach numberandSupercritical airfoils
However, in Chapter two (Two-Dimential subsonic
and
supersonic
equation)
solution
which
of
the
includes:
linearized
Effects
of
.compressibility, Linearized theory
In
the
Chapter
threewith
the
title:
(Small
Disturbance Theory) includes: Centered Prandtel-
Meyer rereflction,Wave Interactions, including:
(Oblique shock reflected from a wall, Oblique
shock
intersection),
Shock
strengthening,
.Supersonic flow over airfoils |
en_US |
dc.description.sponsorship |
Sudan University of Science and Technology |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
Sudan University of Science and Technology |
en_US |
dc.subject |
Mathematics |
en_US |
dc.subject |
Dimential subsonic |
en_US |
dc.subject |
Supersonic |
en_US |
dc.subject |
Hypersonic |
en_US |
dc.title |
A STUDY SUBSONIC AND HYPERSONIC FLOW ON AN AIRFOIL |
en_US |
dc.type |
Thesis |
en_US |