Aeroelastic Characteristics of a Rapid Prototype Multi-Material Wind Tunnel Model of a Mechanically Deployable Aerodynamic Decelerator

Raskin, Boris.
2017-04-19T18:07:42.215Z

Abstract: Scaled wind tunnel models are necessary for the development of aircraft and spacecraft to simulate aerodynamic behavior. This allows for testing multiple iterations of a design before more expensive full-scale aircraft and spacecraft are built. However, the cost of building wind tunnel models can still be high because they normally require costly subtractive manufacturing processes, such... read more

Subjects
Tufts University. Department of Mechanical Engineering.
Permanent URL
http://hdl.handle.net/10427/011805
ID: tufts:21280
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