Using the Maslen method find the change in the shock angle at the nose of a cone
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Using the Maslen method find the change in the shock angle at the nose of a cone pitching with about its nose with a small amplitude. Use body attached coordinate system as done in Example 7.1.
Example 7.1
The surface equation of a body is given by \(\mathrm{z}=\mathrm{a}(\mathrm{x} / l)^{1 / 2,} 0 \leq x \leq l\). If this body pitches by \(\alpha=\bar{\alpha} \sin \omega t\) about its nose in small amplitudes, find the surface pressure variation with time.
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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