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

Download or Read eBook The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow PDF written by Arthur L. Jones and published by . This book was released on 1948 with total page 644 pages. Available in PDF, EPUB and Kindle.
The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
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Total Pages : 644
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ISBN-10 : STANFORD:36105024795648
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Book Synopsis The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow by : Arthur L. Jones

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


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The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Language: en
Pages: 644
Authors: Arthur L. Jones
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1948 - Publisher:

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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
Language: en
Pages: 72
Authors: Arthur Leslie Jones
Categories: Aerodynamics, Supersonic
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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
Language: en
Pages: 756
Authors: Franklin Moore
Categories: Aerodynamics, Supersonic
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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
Language: en
Pages: 64
Authors: Seymour Lampert
Categories: Aerodynamics, Supersonic
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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