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Search Results - christoph+hader
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Control (Delay or Accelerate) Hypersonic Boundary-Layer Transition
This invention is novel flow control techniques for modifying the natural to turbulent transition process of the flow in the boundary layer of vehicles, projectiles, or missiles at supersonic/hypersonic speeds. This invention is concerned with delaying the onset of transition and the subsequent breakdown to turbulence as far downstream on the vehicle...
Published: 8/1/2024
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Inventor(s):
Hermann Fasel
,
Christoph Hader
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Category(s):
Technology Classifications > Engineering & Physical Sciences > Aerospace Engineering