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summary
Estimation of sideforce, yawing moment and rolling moment derivatives due to rate of yaw for complete aircraft at subsonic speeds.
Details
Publisher
ESDU
File size
697.93 KB
Pages
54
Format
PDF
Publication date
1984
ISBN-13
978-2-074-90515-3
ISBN-13 plain
9782074905153
ISBN-10
2074905151