Effects Of Wing Planform On The Aerodynamic Characteristics Of A Wing Body Tail Model At Mach Numbers 157 216 And 287
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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87
| Author | : Royce L. McKinney |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1965 |
| Genre | : Aerodynamic load |
| ISBN | : |
Introduction to Aircraft Flight Mechanics
| Author | : Thomas R. Yechout |
| Publisher | : AIAA |
| Total Pages | : 666 |
| Release | : 2003 |
| Genre | : Aerodynamics |
| ISBN | : 9781600860782 |
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 Stability and Automatic Control
| Author | : Robert C. Nelson |
| Publisher | : |
| Total Pages | : 464 |
| Release | : 1998 |
| Genre | : History |
| ISBN | : |
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Fundamentals of Airplane Flight Mechanics
| Author | : David G. Hull |
| Publisher | : Springer Science & Business Media |
| Total Pages | : 311 |
| Release | : 2007-01-20 |
| Genre | : Technology & Engineering |
| ISBN | : 3540465731 |
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This volume details the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
Aeroacoustics of Flight Vehicles
| Author | : Harvey H. Hubbard |
| Publisher | : |
| Total Pages | : 620 |
| Release | : 1991 |
| Genre | : Aerodynamic noise |
| ISBN | : |
Aerodynamics of V/STOL Flight
| Author | : Barnes Warnock McCormick |
| Publisher | : Courier Corporation |
| Total Pages | : 356 |
| Release | : 1999-01-01 |
| Genre | : Technology & Engineering |
| ISBN | : 9780486404608 |
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds
| Author | : Albert G. Few |
| Publisher | : |
| Total Pages | : 80 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
Dynamics of Flight
| Author | : Bernard Etkin |
| Publisher | : John Wiley & Sons |
| Total Pages | : 392 |
| Release | : 1982 |
| Genre | : Technology & Engineering |
| ISBN | : |
