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Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips : supersonic leading and trailing edges

Isabella J Cole, Kenneth Margolis

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Abstract

the variations of the total pitch~-moment derivative c% + c% ~t$h % wing geometry and Mach number; these calculations sre applicable to slowly (first-order frequency) oscil.latingw~s. .

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the variations of the total pitch~-moment derivative c% + c% ~t$h % wing geometry and Mach number; these calculations sre applicable to slowly (first-order frequency) oscil.latingw~s. .

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Available abstract

the variations of the total pitch~-moment derivative c% + c% ~t$h % wing geometry and Mach number; these calculations sre applicable to slowly (first-order frequency) oscil.latingw~s. .

Key concepts: Supersonic speed, Lift (data mining), Pitching moment, Mechanics, Angle of attack, Acceleration, Physics, Constant (computer programming)

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Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips : supersonic leading and trailing edges — Research Paper | ScholarLens