Author: Royce L. McKinneyPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
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. McKinneyPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
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. FerynIntroduction to Aircraft Flight Mechanics
Author: Thomas R. YechoutPublisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
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 Stability and Automatic Control
Author: Robert C. NelsonPublisher:
ISBN:
Category : History
Languages : en
Pages : 464
Book Description
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. HullPublisher: Springer Science & Business Media
ISBN: 3540465731
Category : Technology & Engineering
Languages : en
Pages : 311
Book Description
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.
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. TreonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Aeroacoustics of Flight Vehicles
Author: Harvey H. HubbardPublisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620
Book Description
Aerodynamics of V/STOL Flight
Author: Barnes Warnock McCormickPublisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356
Book Description
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.
Dynamics of Flight
Author: Bernard EtkinPublisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 392
Book Description
Summary of Low Speed Airfoil Data
Author: Michael S. SeligPublisher: Soartech
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 320
Book Description