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   <subfield code="a">Aerodynamics for engineering students</subfield>
   <subfield code="h">[electronic resource] /</subfield>
   <subfield code="c">E.L. Houghton ... [et al.].</subfield>
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   <subfield code="a">6th ed.</subfield>
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   <subfield code="a">Waltham, MA :</subfield>
   <subfield code="b">Butterworth-Heinemann,</subfield>
   <subfield code="c">2012.</subfield>
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   <subfield code="a">xv, 724 p. :</subfield>
   <subfield code="b">ill. ;</subfield>
   <subfield code="c">24 cm.</subfield>
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   <subfield code="a">Electronic reproduction.</subfield>
   <subfield code="b">Amsterdam :</subfield>
   <subfield code="c">Elsevier Science &amp; Technology,</subfield>
   <subfield code="d">2012.</subfield>
   <subfield code="n">Mode of access: World Wide Web.</subfield>
   <subfield code="n">System requirements: Web browser.</subfield>
   <subfield code="n">Title from title screen (viewed on Apr. 4, 2012).</subfield>
   <subfield code="n">Access may be restricted to users at subscribing institutions.</subfield>
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   <subfield code="a">Already one of the leading course texts on aerodynamics in the UK, the sixth edition welcomes a new US-based author team to keep the text current. The sixth edition has been revised to include the latest developments in compressible flow, computational fluid dynamics, and contemporary applications. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and new examples of 'the aerodynamics around you' have been added to link theory to practical understanding. NEW: Expanded coverage of compressible flow NEW: MATLAB(r) exercises throughout, to give students practice is using industry-standard computational tools. m-files available for download from companion website. NEW: contemporary applications and examples help students see the link between everyday physical examples of aerodynamics and the application of aerodynamic principles to aerodynamic design. NEW: additional examples and end of chapter exercises provide more problem-solving practice for students NEW: improved teaching support with powerpoint slides, solutions manual, m-files, and other resources to accompany the text.</subfield>
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   <subfield code="a">Chapter 1: Basic Concepts and Definitions Chapter 2: Governing equations of fluid mechanics Chapter 3: Potential flow Chapter 4: Two-dimensional wing theory Chapter 5: Finite wing theory Chapter 6: Compressible flow: Part I Chapter 7: Compressible flow: Part II Chapter 8: Viscous flow and boundary layers Chapter 9: Flow control and wing design Chapter 10: Propellers and propulsion Appendices Bibliography Index.</subfield>
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   <subfield code="t">Preface --</subfield>
   <subfield code="g">ch. 1.</subfield>
   <subfield code="t">Basic concepts and definitions --</subfield>
   <subfield code="g">ch. 2.</subfield>
   <subfield code="t">Funamental equations of fluid mechanics --</subfield>
   <subfield code="g">ch. 3.</subfield>
   <subfield code="t">Potential flow --</subfield>
   <subfield code="g">ch. 4.</subfield>
   <subfield code="t">Two-dimensional wing theory --</subfield>
   <subfield code="g">ch. 5.</subfield>
   <subfield code="t">Wing theory --</subfield>
   <subfield code="g">ch. 6.</subfield>
   <subfield code="t">Compressible flow --</subfield>
   <subfield code="g">ch. 7.</subfield>
   <subfield code="t">Airfoils and wings in compressible flow --</subfield>
   <subfield code="g">ch. 8.</subfield>
   <subfield code="t">Viscous flow and boundary layers --</subfield>
   <subfield code="g">ch. 9.</subfield>
   <subfield code="t">Flow control and wing design --</subfield>
   <subfield code="g">ch. 10. Propulsion devices --</subfield>
   <subfield code="g">appendix A.</subfield>
   <subfield code="t">Symbols and notation --</subfield>
   <subfield code="g">Appendix B.</subfield>
   <subfield code="t">[Table : altitute (feet), temperature (Rankine), temperature (Fahrenheit), pressure (psl), density (slug/ft^3)] --</subfield>
   <subfield code="g">appendix C.</subfield>
   <subfield code="t">A solution of integrals of the type of Glauert's integral --</subfield>
   <subfield code="g">appendix D.</subfield>
   <subfield code="t">Conversion of Imperial units to Systαeme international (SI) units --</subfield>
   <subfield code="t">Bibliography.</subfield>
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   <subfield code="a">Aerodynamics.</subfield>
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