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Forebody
英音[ ˈfɒˌbɒdɪ ] 美音[ ˈfɔːrˌbɑːdi ]
弹体前部
常用释义
词性释义
n.
弹体前部；船体前半部
例句
全部
Yao
Opera
is
one
of
local
operas of Tanhuang that
belongs
to
Wu
linguistic
system with
its
forebody
being
"
Yuyao
Tanhuang
"
.
姚剧属吴语系滩簧类地方剧种之一，其前身为“余姚滩簧”。
On
the
basis
of the above
,
the
mechanism
is
investigated
by which the chine
forebody
can
delay
delta
wing
vortex
burst
.
在此基础上，对融合体前体延迟翼涡破裂的机理进行了深入探讨。
The
handling
of
complicated
three
-
dimensional
geometry
models
is
described
.
The
calculated
results
for
forebody
and
biconics are presented.
本文描述了复杂的三维几何模型的处理，并给出了前机身及双级锥的计算结果。
A
new
method
of
quickly generating
hypersonic
waverider
forebody
configurations
was
developed
.
发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。
but
it
increases
the
viscous
forebody
drag
including
the skin
friction
drag
and
shock wave
drag
.
但却增大了包含摩擦阻力和激波阻力的粘性前部阻力。
The
method
of
lines
is
used
to compute
conical
solutions
for
the
sharp
conical
nose
of the
forebody
.
前机身尖锥头部的锥型流场使用直线法求解。
In
the
bomb
hangs
the
strength
under
the
function
,
forebody
then
vertical
underneath
,
the
rear
part
lifts
upwardly
.
弹体的阻力中心位于尾部。在炸弹垂力的作用下，弹体前部便垂向下方，尾部向上抬起。
If a
manual
mini
disturbance
is
set
on
the
tip
of
forebody
, the asymmetric vortices
flow
becomes
determinate
.
通过在模型头部设置确定的微人工扰动可以消除这类流动的不确定性。
In
the
forebody
there
is
a
kitchen
.
在房子的前半部分有一个厨房。
Experimental
and
numerical
investigation
of
a
forward
sweep
sidewall
compression
scramjet inlet with
forebody
compression
带前体压缩的前掠侧压式进气道实验及数值研究
Experiment
Study
of
Aerodynamic
Interactions
of
Projectile
with
Jet
from Its
Forebody
弹丸前体喷流的气动力干扰实验研究
An
experimental
study
of
pneumatic
vortex flow
control
on
high
angle
of attack
forebody
model
大迎角前机身模型上涡流气动控制的实验研究
Optimized
design
of
waverider
forebody
derived
from asymmetric
near
-
isentropic
compression
flow
fields
轴对称近似等熵压缩流场的乘波前体优化设计
Flow
Visualization
For
An
Unconventional
Forebody
一个非常规前体机身的流动显示研究
Results
indicate
:
(1)
Most
of the
boundary
layer
of
forebody
is pushed away
from
the
inlet
by
the
design
of the
inlet
aperture
;
结果表明：进气道口面设计能够将绝大部分前体边界层低能流扫离进气口；
Forebody
Compressibility
Research
of
Hypersonic
Vehicle
高超声速飞行器前体压缩性能研究
Computational
investigation
of
slot
blowing
for
fuselage
forebody
flow
control
开缝吹气用于前机身流场控制的计算研究
Study
on the
near
-
field
aerodynamic
characteristics
of
asymmetry
spherical
forebody
of
blunt
body
球心非对称的钝圆头体近区绕流场气动特性分析研究
Research
of
asymmetric
vortex
characteristic
about
forebody
of
slender
wing
and
body
细长翼身组合体前体非对称涡特性研究
Forebody
vortex
control
with
miniature
,
rotatable
nose
-boom
strakes
运用小型可旋转机头缘条边条进行前机身涡流控制