Problem 1: Analyze the canard-wing combination shown in Fig. 1. The canard and wing are madeof the same airfoil section and haveAR AR, S = 0.25, and = 0.45%1. Develop an expression for the moment coefficient about the center of gravity in terms of theshown parameters (, and zg) and the three-dimensional aerodynamic characteristics of theused wing/canard (CL C and CM).2. What is the range of the cg location for this configuration to be statically stable?You may simplify the problem by neglecting the upwash (downwash) effects between the liftingsurfaces and the drag contribution to the moment. You may also assume small angle approximation.Figure 1: Canard-Wing Configuration.

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Answered: Problem 1: Analyze the canard-wing…

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.55P

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