Author: R. D. MilnePublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
The Unsteady Aerodynamic Forces on Deforming, Low Aspect Ratio Wings and Slender Wing-body Combinations
Author: R. D. MilneThe Unsteady Aerodynamic Forces on Deforming, Low Aspect Ratio Wings and Slender Wing-body Combinations Oscillating Harmonically in a Compressible Flow, by R.D. Milne
Author: Ronald D. MilnePublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42
Book Description
THE UNSTEASY AERODYNAMIC FORCES ON DEFORMING, LOW ASPECT RATIO WINGS AND SLENDER WING-BODY COMBINATIONS OSCILLATING HARMONICALLY IN A COMPRESSIBLE FLOW.
Author: Principles of Aeroelasticity
Author: Raymond L. BisplinghoffPublisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545
Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Aerodynamic-center Considerations of Wings and Wing-body Combinations
Author: John E. LamarAerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground
Author: Marvin P. FinkAerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
Author: John R. SpreiterPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646
Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
The Aerodynamics of Low-aspect-ratio Wings and Wing-body Combinations
Author: Alexander H. FlaxApplied Mechanics Reviews
Author: The Potential Theory of Unsteady Supersonic Flow
Author: John Wilder MilesPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 244
Book Description