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Contents
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Beginning
1
Introduction
2
Normal, oblique and expansion waves
3
Flow over airfoils and wings
Toggle Flow over airfoils and wings subsection
3.1
Subsonic flow
3.2
Transonic flow
3.3
Supersonic flow
4
Flows through nozzles and diffusers
Toggle the table of contents
Aerodynamics/Inviscid and compressible flows
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From Wikiversity
<
Aerodynamics
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>back to Chapters
Introduction
Normal, oblique and expansion waves
Flow over airfoils and wings
Subsonic flow
Transonic flow
Transonic flow over an airfoil
Comparison of flow around conventional and supercritical airfoils at transonic speeds
NASA F-8A Crusader Supercritical Wing Aircraft
A modern airliner
A380
,
M
c
r
u
i
s
e
=
0.85
−
0.96
{\displaystyle M_{cruise}=0.85-0.96}
A modern tuboprop military cargo airplane
A400M
,
M
c
r
u
i
s
e
=
0.68
−
0.72
{\displaystyle M_{cruise}=0.68-0.72}
and
M
p
r
o
p
e
l
l
e
r
≈
0.7
−
1.3
{\displaystyle M_{propeller}\approx 0.7-1.3}
NH90 Tactical Transport Helicopter (TTH),
M
p
r
o
p
e
l
l
e
r
≈
0.4
−
0.8
{\displaystyle M_{propeller}\approx 0.4-0.8}
Supersonic flow
Flows through nozzles and diffusers
Category
:
Aerodynamics