CA-AA242B-Hw1-2

CA-AA242B-Hw1-2 - AA 242B: Mechanical Vibrations (Spring...

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AA 242B: Mechanical Vibrations (Spring 2010) Homework #1 - Part 2 Due April 23, 2010 This is the second part of the two-part homework focusing on developing a simpliFed analytical model of the longitudinal dynamics of an aircraft during the rollout phase of landing. Refer to Homework #1 for the deFnition of the model components and for all other information and stated assumptions . In this second part: 1. Adopt the set of kinematic variables shown in ±igure 1 and explained in Table 1. 2. Adopt the force components shown in ±igure 1 and ±igure 2 and explained in Table 2, in addition to any gravity force. 3. Treat the following variables as “control” variables: δ , T , X gn , X gm where the subscripts n and m designate the nose and main landing gears, respec- tively. 1
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applied moments, and kinematic variables. 2
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This note was uploaded on 06/17/2010 for the course AA 242B taught by Professor Charbelfarhat during the Spring '10 term at Stanford.

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CA-AA242B-Hw1-2 - AA 242B: Mechanical Vibrations (Spring...

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