The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Author: Edward C. Polhamus
Publisher:
Published: 1955
Total Pages: 90
ISBN-13:
DOWNLOAD EBOOKA summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.