Wind-tunnel Investigation of the Static and Dynamic-rotary Stability Derivatives of a Flat-top Wing-body Model at Mach Numbers of 2.5, 3.0 and 3.5 PDF Download

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Wind-tunnel Investigation of the Static and Dynamic-rotary Stability Derivatives of a Flat-top Wing-body Model at Mach Numbers of 2.5, 3.0 and 3.5

Wind-tunnel Investigation of the Static and Dynamic-rotary Stability Derivatives of a Flat-top Wing-body Model at Mach Numbers of 2.5, 3.0 and 3.5 PDF Author: Bedford A. Lampkin
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48

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