Consider a helium-filled airship modeled as an ellipsoid of length = 152 m and a circular cross-section with a maximum diameter = 40 m. Consider a airship flying at a velocity of 25 m/s at a standard altitude of 1000 m (look up the corresponding density in Appendix D). The airship is at a small angle of attack such that its lift coefficient is 0.07 (based on the maximum cross- sectional area). If the airship is flying in straight-and-level flight with no acceleration and has a mass of 120,000 kg, how much cargo is it carrying? (Answer to two decimal places) The total cargo that the airship is carrying is metric tonnes.

Consider a helium-filled airship modeled as an ellipsoid of length = 152 m and a circular cross-section with a maximum diameter = 40 m. Consider a airship flying at a velocity of 25 m/s at a standard altitude of 1000 m (look up the corresponding density in Appendix D). The airship is at a small angle of attack such that its lift coefficient is 0.07 (based on the maximum cross- sectional area). If the airship is flying in straight-and-level flight with no acceleration and has a mass of 120,000 kg, how much cargo is it carrying? (Answer to two decimal places) The total cargo that the airship is carrying is metric tonnes.

Name: Density at 1000m is 1.1117 kg/m^3 Consider a helium-filled airship mod
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Description: Density at 1000m is 1.1117 kg/m^3 Consider a helium-filled airship modeled as an ellipsoid of length = 152 m and a circular cross-section with a maximum diameter = 40 m. Consider a airship flying at a velocity of 25 m/s ata standard altitude of 1000

Classical Dynamics of Particles and Systems

5th Edition

ISBN:9780534408961

Author:Stephen T. Thornton, Jerry B. Marion

Publisher:Stephen T. Thornton, Jerry B. Marion

Chapter11: Dynamics Of Rigid Bodies

Section: Chapter Questions

Problem 11.31P

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