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Transition Research Opportunities at Subsonic and Transonic Speeds

  • Percy J. Bobbitt
Part of the ICASE/NASA LaRC Series book series (ICASE/NASA)

Abstract

Substantial progress has been made in a number of areas related to transition physics and applied transition technology in the past decade. This has been most noticeable in the subsonic and transonic speed regimes where improved stability theories and wind-tunnel facilities coupled with state-of-the-art boundary-layer and inviscid-flow codes have stimulated the design of a number of ambitious wind-tunnel and flight experiments. The data base and code validations obtained provide some of the resources required for the design of flight vehicles with large expanses of laminar flow.

Keywords

Reynolds Number Mach Number Wind Tunnel Flow Quality Stability Code 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag New York Inc. 1990

Authors and Affiliations

  • Percy J. Bobbitt
    • 1
  1. 1.NASA Langley Research CenterHamptonUSA

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