Showing items related by title, author, creator and subject.

• Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods 

  Kumar, Brijesh (2018-02-17)

  As flight flutter testing on an airplane progresses to high dynamic pressures and high Mach number region, it becomes very difficult for engineers to predict the level of the remaining stability in a flutter-prone mode and ...

• Study Of Stall Flutter Of An Isolated Blade In A Low Reynolds Number Incompressible Flow 

  Bhat, Shantanu (2015-07-08)

  Highly-loaded turbomachine blades can stall under off-design conditions. In this regime, the flow can separate close to the leading edge of the blade in a periodic manner that can lead to blade vibrations, commonly referred ...

• Flutter Identification and Aeroelastic Stability during Wake Penetration 

  Sudha, U P V

  Demonstration of utter stability over the design envelope and identi fication of safe ight envelope is a prerequisite for operational clearance of any new aircraft design. An important step involved in flight flutter ...