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Contribution of Motion-Induced Camber Effects to Delta Wing Unsteady Aerodynamics.

From National Research Council Canada

AuthorSearch for: 1; Search for: 2
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
  2. Neilson Engineering
FormatText, Article
Access condition
  • available
  • unclassified
  • unlimited
In
  • AIAA Journal of Aircraft.
NRC numberAL-2000-0014
NPARC number8928149
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Record identifierf2db35ca-7b33-443a-aae8-4ed85f890de7
Record created2009-04-23
Record modified2020-04-16
Date modified: