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summary
Contribution of wing planform to derivatives of yawing moment and sideforce due to roll rate at subsonic speeds, (Np)w and (Yp)w
Details
Publisher
ESDU
File size
996.14 KB
Pages
36
Format
PDF
Publication date
2013
ISBN-13
978-0-856-79339-4
ISBN-13 plain
9780856793394
ISBN-10
1344328300