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summary
Contribution of fin and tailplane to sideforce and yawing moment derivatives due to sideslip at supersonic speeds at low angle of attack.
Details
Publisher
ESDU
File size
765.04 KB
Pages
62
Format
PDF
Publication date
1993
ISBN-13
978-2-074-90515-3
ISBN-13 plain
9782074905153
ISBN-10
2074905151
