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  • 1980-1984  (1)
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    Wind-tunnel tests of the XV-15 tilt rotor aircraft (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of aerodynamic and aeroelastic characteristics prior to flight. The tests were undertaken to investigate the aircraft performance, stability, control and structural loads for flight modes from helicopter through transition and airplane mode up to the tunnel capability of 170 knots. Results from these tests are presented.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-TM-81177 , AVRADCOM-TR-80-A-3 , A-8089
    Format: application/pdf
    Location Call Number Expected Availability
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