3 edition of Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft found in the catalog.
Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft
by National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, For sale by the National Technical Information Service] in Edwards, Calif, [Springfield, Va
Written in English
|Statement||Harry R. Chiles and J. Blair Johnson.|
|Series||NASA technical memorandum -- 86732.|
|Contributions||Johnson, J. Blair., Dryden Flight Research Facility.|
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