Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos
Exercise- -Load factor The picture shows the launch state of a missile sliding along the guide rail under the action of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N, the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a roller, ignoring the rolling friction. The launch angle is 0, try to use the above three expressions to calculate the load factor in the X and Y directions. R+RG cos B R₁₁ = Gl₂ ⋅ cos 0 |R₁f=F₁ e1 8. RB h Ꭱ . | RA R₁ = 1½-½ G cose 4 RB 1₁-12 Geose 1. y Sax = ? {a₁ = ? F₁-Gf cos
International Edition---engineering Mechanics: Statics, 4th Edition
4th Edition
ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
Publisher:Andrew Pytel And Jaan Kiusalaas
Chapter7: Dry Friction
Section: Chapter Questions
Problem 7.78P: The figure shows a steel bar being processed by a rolling mill. Given that P=80kN and r =0.016,...
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
Transcribed Image Text:Exercise- -Load factor
The picture shows the launch state of a missile sliding along the guide rail under the action
of thrust P. It is known that the thrust P=450800N, the weight of the missile is G=20000N,
the front leg A is a slider, the sliding friction coefficient is considered, and the rear leg B is a
roller, ignoring the rolling friction. The launch angle is 0, try to use the above three
expressions to calculate the load factor in the X and Y directions.
R+RG cos
B
R₁₁ = Gl₂ ⋅ cos 0
|R₁f=F₁
e1
8.
RB
h
Ꭱ .
|
RA
R₁ = 1½-½ G cose
4
RB
1₁-12 Geose
1.
y
Sax = ?
{a₁ = ?
F₁-Gf cos
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