Aircraft performance and design
WCB/McGraw-Hill, 1999 - 580 σελίδες
Written by one of the most succesful aerospace authors, this new book develops aircraft performance techniques from first principles and applies then to real airplanes. It also address a philosophy of, and techniques for aircraft design. By developing and discussing these two subjects in a single text, the author captures a degree of synergism not found in other texts. The book is written in a conversational style, a trademark of all of John Anderson's texts, to enhance the readers' understanding.
Τι λένε οι χρήστες - Σύνταξη κριτικής
Δεν εντοπίσαμε κριτικές στις συνήθεις τοποθεσίες.
Άλλες εκδόσεις - Προβολή όλων
aerodynamic center aeronautical aircraft airplane design airplane performance altitude angle of attack aspect ratio assume Boeing calculate camber CD,o chapter chord CL)max configuration cruise decreases delta wing denoted drag coefficient drag due drag polar due to lift engine equation Example Figure flap flight path flight velocity flying free-stream ft/s fuselage given airplane given by Eq ground roll Gulfstream Gulfstream IV Hence high-lift increase induced drag jet-propelled airplane L/D)max landing gear leading edge level flight lift coefficient lift slope lift-to-drag ratio Lilienthal load factor Mach number mi/h minimum NACA obtained parasite drag pivot point planform power available propeller-driven airplane propulsion range rate of climb sea level shown in Fig sketched in Fig specific fuel consumption speed straight wing subsonic surface swept wing takeoff thrust available transonic turbofan turbojet variation vertical tail Vmax wave drag wing loading Wright Flyer zero-lift drag