The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

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The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

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The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.

Linearized Supersonic Axially Symmetric Flow about Open-nosed Bodies Obtained by Use of Stream Function

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First-order relations were obtained for attenuation of shock and flow deflection outward along the shock. These relations probably conform closely to physical f

Rolling and Yawing Moments for Swept-back Wings in Sideslip at Supersonic Sppeds

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A method is presented for determining the rolling and yawing moments of swept-back wings in steady sideslip at supersonic speeds. The case treated in particular

Technical Note - National Advisory Committee for Aeronautics

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