Author: Zhengming Wu
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 198
Book Description
Fundamental Studies of Subsonic and Transonic Flow Separation
Author: Zhengming Wu
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 198
Book Description
Publisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 198
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 602
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 602
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Experimental Study on High Subsonic Turbulent Flow Incipient Separation
Author: Jain-Ming Wu
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
Book Description
For flow over a two-dimensional ramp compression corner case, an experimental investigation to determine the incipient separation was carried out at Mach numbers between 0.55 and 0.9 and Reynolds numbers (based on undisturbed boundary layer thickness) between 350,000 and 690,000. Detailed surface pressure, pitot traversing and oil flow data were obtained for each ramp angle case. Two-dimensionality of the ramp compression corners was verified by the surface oil flow. A major finding of this study is that the incipient separation ramp angle is relatively independent of Mach number and Reynolds number within the range studied. The incipient separation ramp angle was found to be about 22.5 degrees.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
Book Description
For flow over a two-dimensional ramp compression corner case, an experimental investigation to determine the incipient separation was carried out at Mach numbers between 0.55 and 0.9 and Reynolds numbers (based on undisturbed boundary layer thickness) between 350,000 and 690,000. Detailed surface pressure, pitot traversing and oil flow data were obtained for each ramp angle case. Two-dimensionality of the ramp compression corners was verified by the surface oil flow. A major finding of this study is that the incipient separation ramp angle is relatively independent of Mach number and Reynolds number within the range studied. The incipient separation ramp angle was found to be about 22.5 degrees.
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 592
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 592
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 540
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 540
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
AGARD Advisory Report
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 140
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 140
Book Description
Boundary-layer Separation on Isolated Boattail Nozzles
Author: William Kelly Abeyounis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Inventory of advanced energy technologies and energy conservation research and development, 1976-1978
Author: Oak Ridge National Laboratory
Publisher:
ISBN:
Category : Energy conservation
Languages : en
Pages : 2238
Book Description
Publisher:
ISBN:
Category : Energy conservation
Languages : en
Pages : 2238
Book Description