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1
A qualitative introduction to static aeroelasticity: controllability, loads and stability.
IHS ESDU
trim
wing
tailplane
rigid
aeroplane
esdu
angle
lift
speed
elevator
flexible
equation
sketch
fuselage
incidence
unswept
camber
aerodynamic
overall
flight
manoeuvre
axis
weight
current
amendment
positive
loads
zero
setting
stability
incremental
lα
steady
flexibility
twist
aft
divergence
typical
configuration
swept
static
structural
increasing
flexw
negative
assumed
coefficient
effects
washout
defined
Year:
2006
Language:
english
File:
PDF, 725 KB
Your tags:
0
/
5.0
english, 2006
2
A qualitative introduction to static aeroelasticity: controllability, loads and stability.
IHS ESDU International
trim
wing
tailplane
rigid
aeroplane
esdu
angle
lift
speed
elevator
flexible
equation
sketch
fuselage
incidence
unswept
camber
aerodynamic
overall
flight
manoeuvre
axis
weight
product
current
issue
observe
amendment
positive
loads
zero
setting
stability
incremental
lα
steady
flexibility
twist
aft
divergence
typical
configuration
swept
static
structural
increasing
flexw
negative
assumed
coefficient
Language:
english
File:
PDF, 911 KB
Your tags:
0
/
5.0
english
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