Muutke küpsiste eelistusi

Elements of Aerodynamics: A Concise Introduction to Physical Concepts [Kõva köide]

(Naval Postgraduate School)
  • Formaat: Hardback, 208 pages, kaal: 726 g
  • Ilmumisaeg: 04-Nov-2022
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119779979
  • ISBN-13: 9781119779971
Teised raamatud teemal:
Elements of Aerodynamics: A Concise Introduction to Physical ConceptsSuurem pilt
  • Formaat: Hardback, 208 pages, kaal: 726 g
  • Ilmumisaeg: 04-Nov-2022
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119779979
  • ISBN-13: 9781119779971
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781119779971.html
"Elements of Aerodynamics provides important and modern topics used in aerodynamic courses to date. Comprised of 11 chapters, the author ? a noted expert on the topic ? greets the reader with an introduction and approach chapter where factors affecting aerodynamic forces are expertly explained alongside the characteristic size and shape of airfoils. This book expertly provides information on topics such as viscous boundary layers, transonic and hypersonic aerodynamics and thin airfoils in supersonic flows. Packed with plenty of examples and problems, this book is supported by an online solutions manual designed for students and researchers alike. Elements of Aerodynamics will take the reader from a learner to a professional with the support of additionalproblems and equations"--

ELEMENTS OF AERODYNAMICS

An accessible and hands-on textbook filled with chapter objectives, examples, practice problems, sample tests, and an online aero-calculator

In Elements of Aerodynamics, Professor Oscar Biblarz delivers a concise and fundamentals-oriented approach to aerodynamics suitable for both undergraduate and graduate-level students. The text offers numerous problems, examples, and check tests, allowing readers to gain and cement their knowledge through hands-on practice.

Using a unique blend of fundamentals, the book provides students with a new approach to high lift airfoils including examples designed to complement the theory. It covers the most vital information on incompressible and compressible flow over two-dimensional and three-dimensional wings. A companion website that includes an interactive aero-calculator and additional student resources makes this a suitable text for online, hybrid, and distance learning.

Readers will also find:

  • A concise introduction to units and notation with discussion of the proper usage of dimensionless coefficients in aerodynamics, featuring descriptions of airflow as an incompressible and compressible low-viscosity medium past streamlined wings
  • Comprehensive re-evaluation of the fundamentals of fluid dynamics, including the differential control volume approach and formulation of lift, drag, and pitching moments for thin, attached boundary layers over slender wings at high angles of attack
  • Practical applications of mass, momentum, and energy relations, derived from Euler’s equation, Bernoulli’s equation, and the Kutta-Joukowski theorem
  • Selected treatment of transonic and hypersonic aerodynamic aspects, including supercritical airfoils, the non-linear small perturbation potential equation, Newtonian theory, and hypersonic lift and drag

Well-suited for students enrolled in an introductory aerodynamics course as part of an engineering program, Elements of Aerodynamics will also earn a place in the libraries of physics students and those interested in basic fluid mechanics.

To the Student ix
Preface xi
About the Companion Website xiii
1 Introduction and Approach
1(16)
1.1 Introduction
1(1)
1.2 Necessary Assumptions
2(1)
1.3 Units
2(2)
1.4 Equation of State and Fluid Properties
4(6)
1.5 Other Concepts
10(7)
Review Questions
11(2)
Problems
13(1)
Glossary of Terms and Symbols
14(3)
2 Fluid Dynamic Fundamentals
17(18)
2.1 Introduction
17(1)
2.2 Objectives
17(1)
2.3 Control Volume Approach
18(4)
2.4 Lift, Drag, and Pitching Moment
22(1)
2.5 Dimensional Analysis
22(7)
2.6 Small Perturbation Theory in Steady Compressible Flows
29(2)
2.7 Summary
31(4)
Problems
32(1)
Check Test
33(2)
3 Dynamics of Incompressible Flows
35(12)
3.1 Introduction
35(1)
3.2 Objectives
35(1)
3.3 Elementary Flows
36(3)
3.4 Circulation
39(2)
3.5 Superposition of Elementary Flows
41(1)
3.6 Theorems of Helmholtz and Kelvin
42(1)
3.7 Real Flows
43(1)
3.8 Summary
44(3)
Problems
45(1)
Check Test
45(2)
4 Mass, Momentum, and Energy Principles
47(12)
4.1 Introduction
47(1)
4.2 Objectives
47(1)
4.3 Bernoulli's Equation
47(2)
4.4 Airspeed Indicator
49(1)
4.5 Kutta-Joukowski Theorem
50(2)
4.6 Pressure-Energy Equation
52(1)
4.7 Enrichment Topics
53(3)
4.8 Summary
56(3)
Problems
57(1)
Check Test
58(1)
5 Thin Airfoils in Two-Dimensional Incompressible Flow
59(16)
5.1 Introduction
59(1)
5.2 Objectives
60(1)
5.3 The Vortex Filament
60(1)
5.4 Thin Airfoil Theory in Incompressible Flow
60(2)
5.5 Symmetric Contribution at Angle of Attack
62(4)
5.6 Camber Contribution at Zero Angle of Attack
66(2)
5.7 Flapped Symmetric Airfoil at Zero Angle of Attack
68(2)
5.8 Enrichment Topics
70(1)
5.9 Summary
71(4)
Problems
71(2)
Check Test
73(2)
6 Thin Wings of Finite Span in Incompressible Flow
75(14)
6.1 Introduction
75(1)
6.2 Objectives
75(1)
6.3 Lifting Line Theory
76(1)
6.4 Downwash Velocity and Elliptic Spanwise Lift Distribution
76(4)
6.5 Experimental Verification Using Drag Polars
80(1)
6.6 Non-elliptic Planforms and Twist
81(1)
6.7 Effects of Lifting Line Theory on Airplane Performance
82(2)
6.8 Enrichment Topics
84(2)
6.9 Summary
86(3)
Problems
87(1)
Check Test
88(1)
7 Viscous Boundary Layers
89(14)
7.1 Introduction
89(1)
7.2 Objectives
89(1)
7.3 The Boundary Layer Concept
90(1)
7.4 Contributions to Drag
91(1)
7.5 Skin-Friction Drag on Airfoils
92(4)
7.6 Approximate Viscous Boundary Layer Profiles
96(3)
7.7 Enrichment Topics
99(1)
7.8 Summary
100(3)
Problems
101(1)
Check Test
102(1)
8 Fundamentals of Compressible Flow
103(18)
8.1 Introduction
103(1)
8.2 Objectives
103(1)
8.3 Speed of Sound and Mach Waves
104(1)
8.4 Steady-State Isentropic Flow
105(1)
8.5 Supersonic Flows
106(6)
8.6 Critical Mach Number
112(2)
8.7 Supersonic Flat-plate Airfoils
114(2)
8.8 Enrichment Topic
116(1)
8.9 Summary
117(4)
Problems
118(1)
Check Test
119(2)
9 Thin Airfoils in Compressible Flow
121(18)
9.1 Introduction
121(1)
9.2 Objectives
121(1)
9.3 Two-Dimensional Compressible Flow Around Thin Airfoils
122(3)
9.4 The Mach Number Dependence
125(4)
9.5 Supersonic Airfoils
129(3)
9.6 Aircraft Wings in Compressible Flow
132(2)
9.7 Enrichment Topic
134(1)
9.8 Summary
135(4)
Problems
136(2)
Check Test
138(1)
10 Transonic and Hypersonic Aerodynamics
139(16)
10.1 Introduction
139(1)
10.2 Objectives
139(1)
10.3 Transonic Flow
140(4)
10.4 Thick Airfoils for High Subsonic and Transonic Flight
144(1)
10.5 Hypersonic Flow
145(5)
10.6 Enrichment Topics
150(2)
10.7 Summary
152(3)
Problems
152(1)
Check Test
153(2)
11 High-Lift Airfoils in Incompressible Flow
155(18)
11.1 Introduction and Approach
155(1)
11.2 Objectives
156(1)
11.3 Nonlinear Thin Airfoil Theory
156(6)
11.4 Pitching Moment at c/4 and the Aerodynamic Center
162(1)
11.5 High-Lift Wing Mechanisms
163(3)
11.6 Finite Wings
166(1)
11.7 Enrichment Topics
166(4)
11.8 Recapitulation
170(3)
Problems
171(1)
Check Test
172(1)
Appendix A Standard Atmosphere SI Units 173(2)
Appendix B Software 175(4)
Appendix C Equations for
Chapters 5 and 6		 179(2)
Selected References 181(2)
Answers to Selected Problems 183(4)
Index 187
Oscar Biblarz is Professor Emeritus in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School, Monterey, California, USA. He has over 35 years experience teaching and researching aerospace propulsion and fluid mechanics. He holds memberships in the AIAA and the APS. He is coauthor of Rocket Propulsion Elements (with George Sutton) and Fundamentals of Gas Dynamics (with R. D. Zucker), both published by Wiley.