The forward motion of an aircraft in level flight is reduced by two kinds of forces | StudySoup
Calculus: Single Variable | 6th Edition | ISBN: 9780470888643 | Authors: Deborah Hughes-Hallett, Andrew M. Gleason, William G. McCallum, Daniel E. Flath, Patti Frazer Lock, David O. Lomen, David Lovelock, & 9 more

Table of Contents

1
A LIBRARY OF FUNCTIONS
1.1
FUNCTIONS AND CHANGE
1.2
EXPONENTIAL FUNCTIONS
1.3
NEW FUNCTIONS FROM OLD
1.4
LOGARITHMIC FUNCTIONS
1.5
TRIGONOMETRIC FUNCTIONS
1.6
POWERS, POLYNOMIALS, AND RATIONAL FUNCTIONS
1.7
INTRODUCTION TO CONTINUITY
1.8
LIMITS

2
KEY CONCEPT: THE DERIVATIVE
2.1
HOW DO WE MEASURE SPEED?
2.2
THE DERIVATIVE AT A POINT
2.3
THE DERIVATIVE FUNCTION
2.4
INTERPRETATIONS OF THE DERIVATIVE
2.5
THE SECOND DERIVATIVE
2.6
DIFFERENTIABILITY

3
SHORT-CUTS TO DIFFERENTIATION
3.1
POWERS AND POLYNOMIALS
3.10
THEOREMS ABOUT DIFFERENTIABLE FUNCTIONS
3.2
THE EXPONENTIAL FUNCTION
3.3
THE PRODUCT AND QUOTIENT RULES
3.4
THE CHAIN RULE
3.5
THE TRIGONOMETRIC FUNCTIONS
3.6
THE CHAIN RULE AND INVERSE FUNCTIONS
3.7
THE CHAIN RULE AND INVERSE FUNCTIONS
3.8
IMPLICIT FUNCTIONS
3.9
HYPERBOLIC FUNCTIONS

4
USING THE DERIVATIVE
4.1
USING FIRST AND SECOND DERIVATIVES
4.2
OPTIMIZATION
4.3
OPTIMIZATION AND MODELING
4.4
FAMILIES OF FUNCTIONS AND MODELING
4.5
APPLICATIONS TO MARGINALITY
4.6
RATES AND RELATED RATES
4.7
LHOPITALS RULE, GROWTH, AND DOMINANCE
4.8
PARAMETRIC EQUATIONS

5
KEY CONCEPT: THE DEFINITE INTEGRAL
5.1
HOW DO WE MEASURE DISTANCE TRAVELED?
5.2
THE DEFINITE INTEGRAL
5.3
THE FUNDAMENTAL THEOREM AND INTERPRETATIONS
5.4
THEOREMS ABOUT DEFINITE INTEGRALS 2

6
CONSTRUCTING ANTIDERIVATIVES
6.1
ANTIDERIVATIVES GRAPHICALLY AND NUMERICALLY
6.2
CONSTRUCTING ANTIDERIVATIVES ANALYTICALLY
6.3
DIFFERENTIAL EQUATIONS AND MOTION
6.4
SECOND FUNDAMENTAL THEOREM OF CALCULUS

7
INTEGRATION
7.1
INTEGRATION BY SUBSTITUTION
7.2
INTEGRATION BY PARTS
7.3
TABLES OF INTEGRALS
7.4
ALGEBRAIC IDENTITIES AND TRIGONOMETRIC SUBSTITUTIONS
7.5
NUMERICAL METHODS FOR DEFINITE INTEGRALS
7.6
IMPROPER INTEGRALS
7.7
COMPARISON OF IMPROPER INTEGRALS

8
USING THE DEFINITE INTEGRAL
8.1
AREAS AND VOLUMES
8.2
APPLICATIONS TO GEOMETRY
8.3
AREA AND ARC LENGTH IN POLAR COORDINATES
8.4
DENSITY AND CENTER OF MASS
8.5
APPLICATIONS TO PHYSICS
8.6
APPLICATIONS TO ECONOMICS
8.7
DISTRIBUTION FUNCTIONS
8.8
PROBABILITY, MEAN, AND MEDIAN

9
SEQUENCES AND SERIES
9.1
SEQUENCES
9.2
GEOMETRIC SERIES
9.3
CONVERGENCE OF SERIES
9.4
TESTS FOR CONVERGENCE
9.5
POWER SERIES AND INTERVAL OF CONVERGENCE

10
APPROXIMATING FUNCTIONS USING SERIES
10.1
TAYLOR POLYNOMIALS
10.2
TAYLOR SERIES
10.3
FINDING AND USING TAYLOR SERIES
10.4
THE ERROR IN TAYLOR POLYNOMIAL APPROXIMATIONS
10.5
FOURIER SERIES

11
DIFFERENTIAL EQUATIONS
11.1
WHAT IS A DIFFERENTIAL EQUATION?
11.2
SLOPE FIELDS
11.3
EULERS METHOD
11.4
SEPARATION OF VARIABLES
11.5
SEPARATION OF VARIABLES
11.6
APPLICATIONS AND MODELING
11.7
THE LOGISTIC MODEL
11.8
SYSTEMS OF DIFFERENTIAL EQUATIONS
11.9
ANALYZING THE PHASE PLANE

Textbook Solutions for Calculus: Single Variable

Chapter 4.3 Problem 52

Question

The forward motion of an aircraft in level flight is reduced by two kinds of forces, known as induced drag and parasite drag. Induced drag is a consequence of the downward deflection of air as the wings produce lift. Parasite drag results from friction between the air and the entire surface of the aircraft. Induced drag is inversely proportional to the square of speed and parasite drag is directly proportional to the square of speed. The sum of induced drag and parasite drag is called total drag. The graph in Figure 4.50 shows a certain aircrafts induced drag and parasite drag functions. (a) Sketch the total drag as a function of air speed. (b) Estimate two different air speeds which each result in a total drag of 1000 pounds. Does the total drag function have an inverse? What about the induced and parasite drag functions? (c) Fuel consumption (in gallons per hour) is roughly proportional to total drag. Suppose you are low on fuel and the control tower has instructed you to enter a circular holding pattern of indefinite duration to await the passage of a storm at your landing field. At what air speed should you fly the holding pattern? Why?

Solution

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The first step in solving 4.3 problem number 52 trying to solve the problem we have to refer to the textbook question: The forward motion of an aircraft in level flight is reduced by two kinds of forces, known as induced drag and parasite drag. Induced drag is a consequence of the downward deflection of air as the wings produce lift. Parasite drag results from friction between the air and the entire surface of the aircraft. Induced drag is inversely proportional to the square of speed and parasite drag is directly proportional to the square of speed. The sum of induced drag and parasite drag is called total drag. The graph in Figure 4.50 shows a certain aircrafts induced drag and parasite drag functions. (a) Sketch the total drag as a function of air speed. (b) Estimate two different air speeds which each result in a total drag of 1000 pounds. Does the total drag function have an inverse? What about the induced and parasite drag functions? (c) Fuel consumption (in gallons per hour) is roughly proportional to total drag. Suppose you are low on fuel and the control tower has instructed you to enter a circular holding pattern of indefinite duration to await the passage of a storm at your landing field. At what air speed should you fly the holding pattern? Why?
From the textbook chapter OPTIMIZATION AND MODELING you will find a few key concepts needed to solve this.

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Title Calculus: Single Variable  6 
Author Deborah Hughes-Hallett, Andrew M. Gleason, William G. McCallum, Daniel E. Flath, Patti Frazer Lock, David O. Lomen, David Lovelock, & 9 more
ISBN 9780470888643

The forward motion of an aircraft in level flight is reduced by two kinds of forces

Chapter 4.3 textbook questions

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