Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63
Author: Maurice O. Feryn
Publisher:
Published: 1966
Total Pages: 36
ISBN-13:
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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:
Published: 1965
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKIntroduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased 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:
Published: 1998
Total Pages: 464
ISBN-13:
DOWNLOAD EBOOKThis 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
Published: 2007-01-20
Total Pages: 311
ISBN-13: 3540465731
DOWNLOAD EBOOKFlight 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.
The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4
Author: Stuart L. Treon
Publisher:
Published: 1960
Total Pages: 36
ISBN-13:
DOWNLOAD EBOOKAeroacoustics of Flight Vehicles
Author: Harvey H. Hubbard
Publisher:
Published: 1991
Total Pages: 620
ISBN-13:
DOWNLOAD EBOOKDynamics of Flight
Author: Bernard Etkin
Publisher: John Wiley & Sons
Published: 1982
Total Pages: 392
ISBN-13:
DOWNLOAD EBOOKAerodynamics of V/STOL Flight
Author: Barnes Warnock McCormick
Publisher: Courier Corporation
Published: 1999-01-01
Total Pages: 356
ISBN-13: 9780486404608
DOWNLOAD EBOOKAn 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:
Published: 1954
Total Pages: 80
ISBN-13:
DOWNLOAD EBOOKThe 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.
