Publication Date:
2019-07-11
Description:
A vane-type angle-of-attack indicator suitable for measurements at both subsonic and supersonic speeds has been developed by the National Advisory Committee for Aeronautics. A brief history is given of the development, and a wind-tunnel calibration of the indicator is presented, together with a discussion of the corrections to be applied to the indicated readings.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-L9F28a
Format:
application/pdf