Author: Henry W. WoolardPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 40
Book Description
A Selective Bibliography on High-angle-of-attack Aerodynamics of Aircraft and Aircraft Components at Subsonic Speeds
Author: Henry W. WoolardPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 40
Book Description
High Angle of Attack Aerodynamics
Author: Josef RomPublisher: Springer Science & Business Media
ISBN: 1461228247
Category : Science
Languages : en
Pages : 408
Book Description
The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
Aircraft Configurations Developing High Lift-drag Ratios at High Supersonic Speeds
Author: A. J. Eggers (Jr.)Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42
Book Description
Summary: The problem of designing an aircraft which will develop high lift-drag ratios in flight at high supersonic speeds is attacked using the elementary principle that the components of the aircraft should be individually and collectively arranged to impart the maximum downward and the minimum forward momentum to the surrounding air. This principle in conjunction with other practical considerations of hypersonic flight leads to the study of configurations for which the body is situated entirely below the wing; that is, flat-top wing-body combinations. Theory indicates that sensibly complete aircraft of this type can be designed to develop lift-drag ratios well in excess of 6.
Flight Stability and Automatic Control
Author: Robert C. NelsonPublisher: WCB/McGraw-Hill
ISBN: 9780071158381
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
Languages : en
Pages : 441
Book Description
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
High Angle-of-attack Aerodynamics
Author: Publisher:
ISBN: 9789283503224
Category : Aerodynamics
Languages : en
Pages : 416
Book Description
R & D Abstracts
Author: Technology Reports Centre (Great Britain)Publisher:
ISBN:
Category :
Languages : en
Pages : 570
Book Description
The Transonic Aerodynamic Characteristics of Two Variable-sweep Airplane Configurations Capable of Low-level Supersonic Attack
Author: Ralph P. BielatPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 56
Book Description
Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics LaboratoryPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 372
Book Description
Theoretical Investigation at Subsonic Speeds of the Flow Ahead of a Slender Inclinded Parabolic-arc Body of Revolution and Correlation with Experimental Data Obtained at Low Speeds
Author: William LetkoPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 64
Book Description
Subsonic linearized theory is used to derive approximate expressions for the incremental pressure coefficient and flow inclination ahead of slender profile-arc bodies of revolution alined (sic) with the stream and at samll angles of attack or sideslip.
Low-speed Aerodynamic Characteristics of a Model of a Hypersonic Research Airplane at Angles of Attack Up to 90 Degrees for a Range of Reynolds Numbers
Author: James S. BowmanPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 66
Book Description