Euro copter 130 F-WGYP Model was remodeled by John McClane to be weaponized. He plans to integrate a Machine Gun and a rocket launcher to the helicopter by using a truss system. The designed truss is presented Figure FE-001. If the machine gun weighs 181.382kgs and the rocket launcher weighs 181.382kgs and were attached to points B and A respectively, Determine the internal forces on the members and all the reactions of the supports.

Euro copter 130 F-WGYP Model was remodeled by John McClane to be weaponized. He plans to integrate a Machine Gun and a rocket launcher to the helicopter by using a truss system. The designed truss is presented Figure FE-001. If the machine gun weighs 181.382kgs and the rocket launcher weighs 181.382kgs and were attached to points B and A respectively, Determine the internal forces on the members and all the reactions of the supports.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

A 6.1 m long steel column is fixed at its base and pinned at the top end. The cross section is a W360×57. The steel has a yield strength oy = 250 MPa. a) Determine the critical load, Per b) What is the maximum column length to ensure failure due to yielding instead of buckling?
It is a system that is composed of combination of interconnected structural elements and is used to support various loadings. Group of answer choices Statically determinate system Structural system Load analysis system Truss system
QUESTION 5 From the given truss shown: If each member of the truss can only carry 105 Kn for Tension Members and 25 Kn for Compression Members What is the maximum value of F that the truss can carry without failure in any member? 3 m A B 4 m 4 m F
I need the answer as soon as possible
2. Determine the force in each member of the platform truss and state if the members are in tension or compression. Approximate each joint as a pin. 8 kN 16 kN 8 kN 3 т 3 т D. 0 000 3 т F 4 m A 4 m Paint X lite
Steel column pinned at both ends has a modulus of elasticity E = 2 x 105 N/mm², moment of inertia I = 90000 mm4, L = 1.75 m, value of Euler's critical load will be
steel The hollow section column, shown in the figure below, has a length of 18 ft, and it is made of steel with a yield strength of 50 ksi. The column is fixed at the bottom and pinned at the top. What is the capacity of this column under a pure compressive loading? |3/4 in 3/4 in 10 in 5 in
A frame structure is shown below. The links connected below is a bar with a 30mm by 60mm in section. Find the Allowable lad P that can be applied so that the stresses will not exceed 100MPa in tension or 80Mpa in compression.
5 5a 5b 5c Alaterally supported beam was designed for flexure. The beam is safe for shear & deflection. The most economical section is W 8 x 13 however the said section is not readily available at the time of the construction. If you are the engineer in charge of the construction what alternative section will be the best replacement? Why? Use: Fy=248 MPa: E=200,000 MPa Designation Ag (mm2) Weight kg/m 1910 19 30 width 24 flange. thickness d (depth) mm 200.41 bf 100.06 W8 x 10 4.32 15 expla'n briefly your cho'ce. (transform your comparative analys's 'nto a narat've form to support your cho'ce) W8 x 13 2477 202.05 101.60 6.48 W6 x 20 3787 157.48 9.27 152.91 102.36 W6 x 16 3058 159.51 10.29 tf Web 5.21 thickness tw Elastic Properties mm 4 Ix x 106 mm 3 Sx x 103 5.84 6.60 6.60 13 16 17 13 126 162 220 167 mm rx 81.79 81.53 67.56 66.04 mm 4 lyx 106 1 1 6 2 mm 3 Sy x 106 17 22 72 36 mm ry 21.36 21.41 38.10244 24.54 Plastic properties mm 3 Zx x 103 145 187 244 192 mm 3 Zyx 103 27 35 110 56…
Determine the design strength of a T- Beam given the following data: b = 700 mm by = 300 mm hf = 100 mm d = 500 mm fe' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.
A rigid bar is carried by deformable steel and aluminum rods as shown in the figure. If P = 95 kN, a = 4 m, and b = 9 m, determine the ratio of the axial deformation of aluminum to steel. (no unit)