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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design

Gerald V. Foster, O. A. Morris

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Abstract

Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing

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Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing

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Available abstract

Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing

Key concepts: Wing, Airplane, Aerodynamics, Mach number, Wing configuration, Aerospace engineering, Variable (mathematics), Wing loading

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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design — Research Paper | ScholarLens