Introduction to Aeronautics: A Design Perspective
The most exciting moment for an aeronautical engineer is when his or her design becomes a working aircraft, the endpoint of a journey that begins in the classroom. This textbook provides the resources that students need to understand the methods and thought processes involved in designing aircraft. Students learn through the use of specific analytical principles and practical examples taught to them through examples, case studies, and corresponding problems to solve. The material in this text book and AeroDYNAMIC 3.0 software (purchased separately) is sufficient to support a university-level course of three to six semester hours. At the U.S. Air Force Academy (USAFA). Chapters 1-6 are used in a three-semester-hour course taught to the entire student body. The material in Chapters 7-10 is taught at USAFA in later course taken only by aeronautical engineering majors. For professors, this textbook comes complete with end-of-chapter homework problems that provide a summary of the concepts and features contained in the chapters. The problems provide students with an excellent opportunity to analyze and synthesize industry examples, ensuring they understand the key concepts and their applications.
Τι λένε οι χρήστες - Σύνταξη κριτικής
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Aerodynamics and Airfoils
12 άλλες ενότητες δεν εμφανίζονται
Άλλες εκδόσεις - Προβολή όλων
acceleration aerodynamic center aeronautical afterburner aircraft design airfoil airliners airplane altitude angle of attack axis Boeing boundary layer calculated camber center of gravity chord components concept configuration constraint analysis control surfaces cruise curve density design features diagram downwash drag coefficient drag polar engine equation Figure flaps flight flow flowfield force freestream ft/s fuel fuel fraction fuselage glide House of Quality increase induced drag L/D)max landing gear leading edge lift coefficient lift-curve slope load factor longitudinal Mach number maximum methods minimum drag mission molecules NACA parasite drag payload performance planform predicted problem propulsion result Reynolds number sea level shown in Fig slug/ft3 span spar stagnation point standard atmosphere strake structural subsonic supersonic takeoff temperature thrust trim True Airspeed TSFC tube turbofan turbojet values velocity vector vertical wave drag weight wing loading zero
Flight Performance of Fixed and Rotary Wing Aircraft
Δεν υπάρχει διαθέσιμη προεπισκόπηση - 2006
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Introduction to Aircraft Flight Mechanics: Performance, Static Stability ...
Steven L. Morris
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