File:CLP avec 4 ailerons de différentes tailles selon Mach , d'après Clark De Jonge.png

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Captions

Position of the Center of Pressure of a rocket with 4 fins of different sizes depending on the Mach, according to Clark De Jonge.

Summary

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Description
Français : Position du Centre de Portance d'une fusée avec 4 ailerons de différentes tailles selon le Mach , d'après Clark De Jonge. Les ailerons ont toujours le même allongement géométrique envergure unitaire / corde. L'ogive de 4 calibres est tangente. D'après "The effect of low aspect ratio rectangular and delta cruciform fins on the stability of bodies of revolution with tangent ogives at small angles of attack through a Mach number range of 0 to 3.5", by Clark De Jonge, Armed Services Technical Information Agency, AD 278 423 [1].
English: Position of the Center of Pressure of a rocket with 4 fins of different sizes depending on the Mach, according to Clark De Jonge. The ailerons always have the same geometric Aspect Ratio unit wingspan / chord. The 4-caliber ogive is tangent. Acording to "The effect of low aspect ratio rectangular and delta cruciform fins on the stability of bodies of revolution with tangent ogives at small angles of attack through a Mach number range of 0 to 3.5", by Clark De Jonge, Armed Services Technical Information Agency, AD 278 423 [2].
Date
Source Own work
Author Bernard de Go Mars

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current11:07, 10 March 2021Thumbnail for version as of 11:07, 10 March 20211,286 × 1,082 (128 KB)Bernard de Go Mars (talk | contribs)Uploaded own work with UploadWizard

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