Author: W. J. McCroskey
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
The addition of heat to the boundary layer of an insulated flat plate by means of a point heat source at the leading edge has been found to delay the transition of laminar flow to turbulence. This paper describes an experimental investigation of the variation of transition Reynolds number on a roughened flat plate model with a heat source of strength, Q, spanning the leading edge. The present problem is compared with the problem of an aerodynamically heated boundary layer on an insulated flat plate. Transition Reynolds number was found to increase with increasing S over a range equivalent to a Mach number variation of 0
Experimental Investigation of Boundary Layer Transition on a Flat Plate with a Point Heat Source at the Leading Edge
Author: W. J. McCroskey
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
The addition of heat to the boundary layer of an insulated flat plate by means of a point heat source at the leading edge has been found to delay the transition of laminar flow to turbulence. This paper describes an experimental investigation of the variation of transition Reynolds number on a roughened flat plate model with a heat source of strength, Q, spanning the leading edge. The present problem is compared with the problem of an aerodynamically heated boundary layer on an insulated flat plate. Transition Reynolds number was found to increase with increasing S over a range equivalent to a Mach number variation of 0
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
The addition of heat to the boundary layer of an insulated flat plate by means of a point heat source at the leading edge has been found to delay the transition of laminar flow to turbulence. This paper describes an experimental investigation of the variation of transition Reynolds number on a roughened flat plate model with a heat source of strength, Q, spanning the leading edge. The present problem is compared with the problem of an aerodynamically heated boundary layer on an insulated flat plate. Transition Reynolds number was found to increase with increasing S over a range equivalent to a Mach number variation of 0
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 1118
Book Description
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 1118
Book Description
An Experimental Investigation of Heat Transfer in the Turbulent Boundary Layer on a Flat Plate Design of Apparatus
Author: Hugh Maxwell Satterlee
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 258
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
Book Description
Instability and Transition
Author: M.Y. Hussaini
Publisher: Springer Science & Business Media
ISBN: 1461234301
Category : Science
Languages : en
Pages : 462
Book Description
These two volumes contain the proceedings of the workshop on the Institute for Computer Instability and Transition, sponsored by Applications in Science and Engineering (ICASE) and the Langley Research Center (LaRC), during May 15 to June 9, 1989. The work shop coincided with the initiation of a new, focused research pro gram on instability and transition at LaRC. The objectives of the workshop were to (i) expose the academic community to current technologically important issues of instability and transition in shear flows over the entire speed range, (ii) acquaint the academic com munity with the unique combination of theoretical, computational and experimental capabilities at LaRC and foster interaction with these facilities, (iii) review current state-of-the-art and propose fu ture directions for instability and transition research, (iv) accelerate progress in elucidating basic understanding of transition phenomena and in transferring this knowledge into improved design methodolo gies through improved transition modeling, and (v) establish mech anisms for continued interaction. The objectives (i) to (iii) were of course immediately met. It is still premature to assess whether ob jectives (iv) and (v) are achieved. The workshop program consisted of tutorials, research presenta tions, panel discussions, experimental and computational demonstra tions, and collaborative projects.
Publisher: Springer Science & Business Media
ISBN: 1461234301
Category : Science
Languages : en
Pages : 462
Book Description
These two volumes contain the proceedings of the workshop on the Institute for Computer Instability and Transition, sponsored by Applications in Science and Engineering (ICASE) and the Langley Research Center (LaRC), during May 15 to June 9, 1989. The work shop coincided with the initiation of a new, focused research pro gram on instability and transition at LaRC. The objectives of the workshop were to (i) expose the academic community to current technologically important issues of instability and transition in shear flows over the entire speed range, (ii) acquaint the academic com munity with the unique combination of theoretical, computational and experimental capabilities at LaRC and foster interaction with these facilities, (iii) review current state-of-the-art and propose fu ture directions for instability and transition research, (iv) accelerate progress in elucidating basic understanding of transition phenomena and in transferring this knowledge into improved design methodolo gies through improved transition modeling, and (v) establish mech anisms for continued interaction. The objectives (i) to (iii) were of course immediately met. It is still premature to assess whether ob jectives (iv) and (v) are achieved. The workshop program consisted of tutorials, research presenta tions, panel discussions, experimental and computational demonstra tions, and collaborative projects.
AFOSR.
Author: United States. Air Force. Office of Scientific Research
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 968
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 968
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 736
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 736
Book Description
AIAA 2nd Shear Flow Conference
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 620
Book Description
Charts for Estimating Boundary-layer Transition on Flat Plates
Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 36
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 48
Book Description