Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Leeward Flow Over Delta Wings at Supersonic Speeds
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Vortex Flows at Supersonic Speeds
Author: Richard M. Wood
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 104
Book Description
Lee-side Flow Over Delta Wings at Supersonic Speeds
Author: David S. Miller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 160
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 160
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 556
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 556
Book Description
Transonic Symposium: Theory, Application, and Experiment
Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 964
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 964
Book Description
Symposium Transsonicum III
Author: Jürgen Zierep
Publisher: Springer Science & Business Media
ISBN: 3642835848
Category : Science
Languages : en
Pages : 503
Book Description
Continuing the tradition of the IUTAM Symposia TRANSSONICA, this review of the numerical simulation and physical modelling of transonic flows presents new developments in the fields of computational and experimental aerodynamics. A major topic of the symposium proceedings is the evaluation of present numerical analysis techniques with respect to transonic aerodynamics. In the field of experimental aerodynamics, the high Reynolds number effect and the interference-free testing in transonic wind tunnels are of special interest.
Publisher: Springer Science & Business Media
ISBN: 3642835848
Category : Science
Languages : en
Pages : 503
Book Description
Continuing the tradition of the IUTAM Symposia TRANSSONICA, this review of the numerical simulation and physical modelling of transonic flows presents new developments in the fields of computational and experimental aerodynamics. A major topic of the symposium proceedings is the evaluation of present numerical analysis techniques with respect to transonic aerodynamics. In the field of experimental aerodynamics, the high Reynolds number effect and the interference-free testing in transonic wind tunnels are of special interest.
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1102
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1102
Book Description
Laser Velocimetry Measurements of Vortex Flows on a Delta Wing at Mach 1.9
Author: Linda G. Smith
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 120
Book Description
Off-body flow visualizations and fluid velocity measurements are conducted in a supersonic vortex flow. Three-dimensional laser velocimetry measurements are made in the leeward flowfield over a simple sharp-edged delta wing with 75 degree sweep angle. Tests are conducted at Mach 1.9 and Reynolds number of 2.4 x 10(exp 6) based on model root chord. Measurements are made at 40% and 80% chord positions for 20 and 30 degree angles of attack and at 40% chord for 35 degrees. Mean velocities and turbulence intensities are measured on the five planes. Measurement accuracy is discussed in detail. The measurements define the location of the vortex core and provide the flowfield velocities surrounding the vortex. The difficulties inherent with seeding high velocity vortex flows are discussed ... Laser Velocimetry Measurement of Vortical Flowfields.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 120
Book Description
Off-body flow visualizations and fluid velocity measurements are conducted in a supersonic vortex flow. Three-dimensional laser velocimetry measurements are made in the leeward flowfield over a simple sharp-edged delta wing with 75 degree sweep angle. Tests are conducted at Mach 1.9 and Reynolds number of 2.4 x 10(exp 6) based on model root chord. Measurements are made at 40% and 80% chord positions for 20 and 30 degree angles of attack and at 40% chord for 35 degrees. Mean velocities and turbulence intensities are measured on the five planes. Measurement accuracy is discussed in detail. The measurements define the location of the vortex core and provide the flowfield velocities surrounding the vortex. The difficulties inherent with seeding high velocity vortex flows are discussed ... Laser Velocimetry Measurement of Vortical Flowfields.
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 542
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 542
Book Description
Experimental Effects of Wing Location on Wing-body Pressures at Supersonic Speeds
Author: Jerry M. Allen
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 204
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 204
Book Description