Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
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Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C.], [Springfield, Va .
Written in English

Subjects:

  • Air flow.,
  • Angle of attack.,
  • Engine inlets.,
  • F-18 aircraft.,
  • Flow distribution.,
  • Inlet flow.,
  • Intake systems.,
  • Wind tunnel tests.,
  • Wind tunnel walls.,
  • Wind tunnels.

Book details:

Edition Notes

StatementCrawford F. Smith.
SeriesNASA contractor report -- 195429., NASA contractor report -- NASA CR-195429.
ContributionsUnited States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15409179M

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