'Aerodynamic loads' presentation slideshows

Research & Development

Research & Development. Wind Tunnel Testing Needs to be applicable for subsonic, transonic, and supersonic velocities Scaled down model Associated costs Dimensions to minimize error due to scale effects, flow blockage, and wall boundary layers Possible testing locations

475 views • 39 slides

Research & Development

Research & Development. Wind Tunnel Testing Needs to be applicable for subsonic, transonic, and supersonic velocities Scaled down model Associated costs Dimensions to minimize error due to scale effects, flow blockage, and wall boundary layers Possible testing locations

396 views • 39 slides

Simulating an Insect-Scale Flapping Wing Air Vehicle

847 views • 31 slides

Progress Presentation ARDB Aircraft Systems Panel October 22, 2002 RCI, Hyderabad

Progress Presentation ARDB Aircraft Systems Panel October 22, 2002 RCI, Hyderabad Centre for Aerospace Systems Design & Engineering Indian Institute of Technology Bombay. Objectives, Mission. SDE Education Multi-disciplinary Design Optimisation System Level Studies.

331 views • 16 slides