Answer questions 6.23 and 6.24 which is its continuation laded Purchased from American Institute of Aeronautics and Astronautics300INTRODUCTION TO AIROCRAFT FLIGHT MECHANICS6.19 An aircraft has a lift curve slope of 0.10/deg and a Cm. = -0.04/deg.What is the aircraft's static margin?6.20 An aircraft has longitudinal static stability at a given center of gravitylocation. Which of the following is true?(a) the static margin is negative(b) d8/aC = 0(c) Cm. < 0т,(d) all of the above6.21 Assume a Lear Jet is cruising (level, unaccelerated flight) at 40,000 ftwith U = 677 ft/s, S = 230 ft’, Weight=13,000lb, and CT = 0.0335.Find CL, and CD,6.22 Compute the thrust being produced by the Lear Jet in Problem 6.21.6.23 Given f(x) =f(a) +f'(a)(x – a) and f(z) = –0.1x* – 0.15x³ – 0.5x²–0.25x + 1.2Use the first-order Taylor series approximation to evaluate f(x) givenf(a) where:a = 1x= 26.24 Compare the answer from Problem 6.23 with what you would obtain justevaluating f(a) at a = 2.6.25 To obtain the same answer for Problems 6.23 and 6.24, what orderTaylor series would you use? Try it.

We have to approximate the f(x).

Compute the thrust being produced by the Lear Jet in Problem 6.21. Given f(x) =f(a) +f'(a)(x – a) and f(z) = –0.1x* – 0.15x – 0.5x²– .25x + 1.2 Use the first-order Taylor series approximation to evaluate f(x) given (a) where: - a = 1 x= 2 Compare the answer from Problem 6.23 with what you would obtain just evaluating f(a) at a = 2.

Compute the thrust being produced by the Lear Jet in Problem 6.21. Given f(x) =f(a) +f'(a)(x – a) and f(z) = –0.1x* – 0.15x – 0.5x²– .25x + 1.2 Use the first-order Taylor series approximation to evaluate f(x) given (a) where: - a = 1 x= 2 Compare the answer from Problem 6.23 with what you would obtain just evaluating f(a) at a = 2.

Linear Algebra: A Modern Introduction

4th Edition

ISBN:9781285463247

Author:David Poole

Publisher:David Poole

Chapter1: Vectors

Section1.4: Applications

Problem 9EQ

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