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Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results

H. J. Walker, C. H. Wolowicz

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Abstract

Longitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing

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Longitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing

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Available abstract

Longitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing

Key concepts: Airplane, Supersonic speed, Wind tunnel, Aerospace engineering, Hypersonic flight, Hypersonic speed, Aeronautics, Stability (learning theory)

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Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results — Research Paper | ScholarLens