2 options
Reynolds number effects on the performance of lateral control devices / Raymond E. Mineck.
- Format:
- Book
- Government document
- Author/Creator:
- Mineck, Raymond E., author.
- Series:
- NASA technical memorandum ; 2000-210541.
- NASA/TM ; 2000-210541
- Language:
- English
- Subjects (All):
- Ailerons.
- Reynolds number.
- Spoilers (Airplanes).
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (139 pages) : illustrations.
- Place of Publication:
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2000.
- Summary:
- The influence of Reynolds number on the performance of outboard spoilers and ailerons was investigated on a generic subsonic transport configuration in the National Transonic facility over a chord Reynolds number range from 3x100000 to 30 x1000000 and a Mach number range from 0.50 to 0.94. Spoiler deflection angles of 0°, 10°, 15° and 20° and aileron deflection angles of -10°, 0° and 10° were tested. Aeroelastic effects were minimized by testing at constant normalized dynamic presuure conditions over intermediate Reynolds number ranges.
- Notes:
- "October 2000."
- "Performing organization: NASA Langley Research Center"--Report documentation page.
- Includes bibliographical references (page 43).
- Online resource; title from PDF title page (NASA, viewed Nov. 6, 2017).
- Other Format:
- Print version: Mineck, Raymond E. Reynolds number effects on the performance of lateral control devices
- Microfiche version: Mineck, Raymond E. Reynolds number effects on the performance of lateral control devices
- OCLC:
- 858278714
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