The Effects of Sideslip Aspect Ratio and Mach Number on the Lift and Pitching Moment of Triangular Trapezoidal and Related Plan Forms in Supersonic Flow is popular PDF and ePub book, written by Arthur L. Jones in 1949, it is a fantastic choice for those who relish reading online the Aerofoils genre. Let's immerse ourselves in this engaging Aerofoils book by exploring the summary and details provided below. Remember, The Effects of Sideslip Aspect Ratio and Mach Number on the Lift and Pitching Moment of Triangular Trapezoidal and Related Plan Forms in Supersonic Flow can be Read Online from any device for your convenience.
The Effects of Sideslip Aspect Ratio and Mach Number on the Lift and Pitching Moment of Triangular Trapezoidal and Related Plan Forms in Supersonic Flow Book PDF Summary
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.
Detail Book of The Effects of Sideslip Aspect Ratio and Mach Number on the Lift and Pitching Moment of Triangular Trapezoidal and Related Plan Forms in Supersonic Flow PDF
- Author : Arthur L. Jones
- Release : 01 October 2024
- Publisher : Unknown
- ISBN : UOM:39015086494054
- Genre : Aerofoils
- Total Page : 78 pages
- Language : English
- PDF File Size : 21,8 Mb
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