The profile given in Problem 7.12. is in plunging motion with (mathrm{k}=0.3). Determine the upper surface pressure

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The profile given in Problem 7.12. is in plunging motion with $\mathrm{k}=0.3$. Determine the upper surface pressure distribution in terms of the amplitude of plunging.

Problem 7.12

For a 5% thick airfoil find the free stream Mach number for which:

(i) first order,

(ii) second order

(iii) third order piston theory is applicable.

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Fundamentals Of Modern Unsteady Aerodynamics

ISBN: 9783030607760,9783030607777

3rd Edition

Authors: Ülgen Gülçat

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Question Posted: Apr 17, 2024 04:09 AM

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The profile given in Problem 7.12. is in plunging motion with (mathrm{k}=0.3). Determine the upper surface pressure

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Fundamentals Of Modern Unsteady Aerodynamics

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