Aerodynamic Principles of Flight Vehicles


Book Description

In "Aerodynamic Principles of Flight Vehicles" Argyris Panaras examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, to the evolution of flight vehicle shapes as flight speed has increased, and to discoveries that enabled breakthrough developments in flight. The book: examines why various equations and technologies were developed, explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave-boundary layer interactions, among others, and helps readers apply concepts from the material to their own projects. Archival and encyclopedic, "Aerodynamic Principles of Flight Vehicles" is a superb reference for aeronautical students and professionals alike. Although most beneficial to readers with a working knowledge of aerodynamics, it is accessible to anyone with an introductory understanding of the field.




Mach 1 and Beyond: The Illustrated Guide to High-Speed Flight


Book Description

Publisher's Note: Products purchased from Third Party sellers are not guaranteed by the publisher for quality, authenticity, or access to any online entitlements included with the product. This compelling book opens up the world of high-speed flight to readers who do not have extensive technical backgrounds Covering both subsonic and supersonic flight, it demystifies the world of high-speed aerodynamics, flight principles, gas turbine jets, and more. You'll learn why there are no supersonic airliners, what problems confront designers of 2,000-mph aircraft, and whether or not a hypersonic, or Mach 5, airplane is likely to be built.




Aircraft Flight


Book Description

This book is intended to provide a description on the principles of aircraft flight in physical rather than mathematical terms. The authors have included some of the more important practical aspects of aircraft flight plus examples of innovations, descriptions of which are generally only found scattered in assorted technical journals. two simple formulae as a means of defining important terms such as lift coefficient and Reynolds number, which are essential to the understanding of aeronautics. important, or interesting. They have also restricted coverage to the aerodynamics and mechanics of flight, with only a brief consideration of other aspects such as structural influences. interested in aircraft or contemplating a career in aeronautics. Students of aeronautical engineering should find it helpful as introductory and background reading. It should also be useful to employees in the industry such as flight crew and ground staff. physical science and is at least vaguely familiar with concepts such as energy and momentum.




Aircraft Flight


Book Description




Understanding Flight


Book Description

The simplest, most intuitive book on the toughest lessons of flight--addresses the science of flying in terms, explanations, and illustrations that make sense to those who most need to understand: those who fly. Debunks long-rooted misconceptions and offers a clear, minimal-math presentation that starts with how airplanes fly and goes on to clarify a diverse range of topics, such as design, propulsion, performance, high-speed flight, and flight testing. Not-to-be missed insights for pilots, instructors, flight students, aeronautical engineering students, and flight enthusiasts.




Introduction to Aircraft Flight Mechanics


Book Description

Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.




Flight Theory and Aerodynamics


Book Description

The classic text for pilots on flight theory and aerodynamics?now in an updated Second Edition Flight Theory and Aerodynamics, the basic aeronautics text used by the United States Air Force in their Flying Safety Officer course, is the book that brings the science of flight into the cockpit. Designed for the student with little engineering or mathematical background, the book outlines the basic principles of aerodynamics and physics, using only a minimal amount of high school?level algebra and trigonometry necessary to illustrate key concepts. This expanded seventeen chapter Second Edition reflects the cutting edge of aeronautic theory and practice, and has been revised, reorganized, and updated with 30% new information?including a new chapter on helicopter flight. Central to the book?s structure is a clear description of aeronautic basics?what lifts and drives an aircraft, and what forces work for and against it?all detailed in the context of the design and analysis of today?s aircraft systems: Atmosphere and airspeed measurement Airfoils and aerodynamic forces Lift and drag Jet aircraft basic and applied performance Prop aircraft basic and applied performance Slow and high-speed flight Takeoff, landing, and maneuvering performance The book?s practical, self-study format includes problems at the end of each chapter, with answers at the back of the book, as well as chapter-end summaries of symbols and equations. An ideal text for the USN Aviation Safety Officer and the USAAA?s Aviation Safety Officer courses, as well as for professional pilots, student pilots, and flying safety personnel, Flight Theory and Aerodynamics is a complete and accessible guide to the subject, updated for the new millennium.




Aerodynamics Principles for Air Transport Pilots


Book Description

Equipping readers with the ability to analyze the aerodynamic forces on an aircraft, the book provides comprehensive knowledge of the characteristics of subsonic and supersonic airflow. This book begins with the fundamental physics principles of aerodynamics, then introduces the Continuity Equation, Energy Equations, and Bernoulli’s Equation, which form the basic aerodynamic principles for subsonic airflow. It provides a thorough understanding of the forces acting on an aircraft across a range of speeds and their effects on the aircraft's performance, including a discussion on the difference in aerofoil and aircraft shapes. Aircraft stability issues are analyzed, along with the development of a boundary layer over an aerofoil, the changes of air speed and air pressure, and boundary layer separation. Readers will gain a clear understanding of the nature of airflow over aircraft during subsonic, transonic, and supersonic flight. The book emphasizes the connection between operating actions in flight and aerodynamic requirements. The content will be of interest to senior undergraduates studying to obtain their Airline Transport Pilot License (ATPL)/Airline Transport Pilot (ATP) certificate, general aviation and air transport pilots, and aircraft maintenance engineers.