2.6. An airplane has the following pitching moment characteristics at the center of gravity position: Xog/= 0.3. Ста = Сто + JC CL dC₁ + Cm 8 JC where C = 0.05 = -0.1 Cm = -0.01/deg dCL S-M-M If the airplane is loaded so that the center of gravity position moves to x/= 0.10, can the airplane be trimmed during landing, C₁ = 1.0? Assume that Cand Care unaffected by the center of gravity travel and that 8 = ±20°.

International Edition---engineering Mechanics: Statics, 4th Edition
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ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
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Chapter8: Centroids And Distributed Loads
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Problem 8.90P: The hemispherical glass bowl is filled with water. Find the location y of the center of gravity of...
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2.6. An airplane has the following pitching moment characteristics at the center of gravity
position:
Xog/= 0.3.
Ста = Сто
+
JC CL
dC₁
+ Cm 8
JC
where
C = 0.05
= -0.1 Cm = -0.01/deg
dCL
S-M-M
If the airplane is loaded so that the center of gravity position moves to x/= 0.10,
can the airplane be trimmed during landing, C₁ = 1.0? Assume that Cand Care
unaffected by the center of gravity travel and that 8 = ±20°.
Transcribed Image Text:2.6. An airplane has the following pitching moment characteristics at the center of gravity position: Xog/= 0.3. Ста = Сто + JC CL dC₁ + Cm 8 JC where C = 0.05 = -0.1 Cm = -0.01/deg dCL S-M-M If the airplane is loaded so that the center of gravity position moves to x/= 0.10, can the airplane be trimmed during landing, C₁ = 1.0? Assume that Cand Care unaffected by the center of gravity travel and that 8 = ±20°.
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