Information Centre for Aeronautics nakladatelství

Knihy (4)

 A Discontinuity in Fatigue S/N Curve
Application of Several Methods Based on Least-Squares Principle for Determining Longitudinal Aerodynamic Derivatives of Aeroplane from Flight Test Data(Summary report)
Boundary-Lay er Development on a Wing-Body CombinationSummary Report
On Aircraft Longitudinal Motion After Boundary Layer Control System Failure During Take-Off and Landing(Summary report)

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