-AB cos(T/3) + AC + Ax = 0 -AB sin(7/3) + Ay = 0 AB cos(7/3) – BC cos (T/3)- BD = 0 AB sin(T/3) + BC sin(t/3) = W/2 -AC + BC cos(Tt/3) – CD cos(T/3) + CE = 0 -BC sin(t/3) – CD sin(t/3) = 0 BD + CD cos(t/3) - DE cos(t/3) = 0 CD sin(r/3) +DE sin(t/3) = W/2 DE cos(T/3) – CE = 0 -DE sin(t/3) + Ey = 0 where AB, AC, BC, etc. are the axial forces carried by the members, W is the weight of the fuel-filled rocket, Ax and Ay are the x- and y- components of the reaction force at joint A, and Ey is the reaction force at joint E, and angles are in units of radians. The axial stress in each member of the truss will be o (axial force)/(cross-sectional area).

Understanding Motor Controls
4th Edition
ISBN:9781337798686
Author:Stephen L. Herman
Publisher:Stephen L. Herman
Chapter53: The 555 Timer
Section: Chapter Questions
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How would you put this into vector form.
-AB cos(T/3) + AC+ Ax = 0
-AB sin(7/3) + Ay = 0
AB cos(T/3)- BC cos (T/3)-BD 0
AB sin(a/3) + BC sin(7/3) = W/2
-AC + BC cos(t/3) - CD cos(T/3)+CE 0
-BC sin(/3) – CD sin(t/3) = 0
BD + CD cos(T/3)- DE cos(t/3) = 0
CD sin(T/3) + DE sin(t/3) = W/2
DE cos(T/3) – CE = 0
-DE sin(r/3) + Ey= 0
where AB, AC, BC, etc. are the axial forces carried by the members, W is the weight of the fuel-filled
rocket, Ax and Ay are the x- and y- components of the reaction force at joint A, and Ey is the reaction force
at joint E, and angles are in units of radians. The axial stress in each member of the truss will be o3 (axial
force)/(cross-sectional area).
Transcribed Image Text:-AB cos(T/3) + AC+ Ax = 0 -AB sin(7/3) + Ay = 0 AB cos(T/3)- BC cos (T/3)-BD 0 AB sin(a/3) + BC sin(7/3) = W/2 -AC + BC cos(t/3) - CD cos(T/3)+CE 0 -BC sin(/3) – CD sin(t/3) = 0 BD + CD cos(T/3)- DE cos(t/3) = 0 CD sin(T/3) + DE sin(t/3) = W/2 DE cos(T/3) – CE = 0 -DE sin(r/3) + Ey= 0 where AB, AC, BC, etc. are the axial forces carried by the members, W is the weight of the fuel-filled rocket, Ax and Ay are the x- and y- components of the reaction force at joint A, and Ey is the reaction force at joint E, and angles are in units of radians. The axial stress in each member of the truss will be o3 (axial force)/(cross-sectional area).
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