Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate

DOWNLOAD

Download Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page

Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate

DOWNLOAD
Author : Don W. Jillie
language : en
Publisher:
Release Date : 1961

Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate written by Don W. Jillie and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Fluid mechanics categories.

Nasa Technical Note

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1970

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.

Charts For Estimating Boundary Layer Transition On Flat Plates

DOWNLOAD
Author : Edward J. Hopkins
language : en
Publisher:
Release Date : 1970

Charts For Estimating Boundary Layer Transition On Flat Plates written by Edward J. Hopkins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Boundary layer categories.

Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate

DOWNLOAD
Author : DON W. JILLIE
language : en
Publisher:
Release Date : 1961

Effects Of Mach Number Leading Edge Bluntness And Sweep On Boundary Layer Transition On A Flat Plate written by DON W. JILLIE and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

The effects of leading-edge bluntness and sweep on boundary-layer transition on flat plate models were investigated at Mach numbers of 2.00, 2.50, 3.00, and 4.00. The effect of sweep on transition was also determined on a flat plate model equipped with an elliptical nose at a Mach number of 0.27. Models used for the supersonic investigation had leading-edge radii varying from 0.0005 to 0.040 inch. The free-stream unit Reynolds number was held constant at 15 million per foot for the supersonic tests and the angle of attack was 0 degrees. Surface flow conditions were determined by visual observation and recorded photographically. For the models with the blunter leading edges, the transition Reynolds number (based on free-stream flow conditions) was approximately doubled by an increase in Mach number from 2.50 to 4.00; and nearly the same result was predicted from shock-loss considerations. At all supersonic Mach numbers, increases in sweep reduced the transition Reynolds number and the amount of reduction increased with increases in bluntness. The shock-loss method considerably underestimated the sweep effects, with swept wings. (Author).

Index Of N A S A Technical Publications

DOWNLOAD
Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960

Index Of N A S A Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.

A Selected Listing Of Nasa Scientific And Technical Reports For

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1960

A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.

Separation Ahead Of Controls On Swept Wings

DOWNLOAD
Author : Kaufman Louis G. (II)
language : en
Publisher:
Release Date : 1975

Separation Ahead Of Controls On Swept Wings written by Kaufman Louis G. (II) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics, Hypersonic categories.

Shock-induced flow-separation ahead of trailing edge controls on swept wings is investigated with emphasis on the effects of boundary layer transition on the location and shape of the separation line. Experimental results were obtained by using forward facing steps mounted on swept-leading-edge flat-plate wing models in the ARL Mach 6 Tunnel for model running length Reynolds numbers varying from 0.9 to 33 million. The data support qualitatively a proposed, strip-type method for estimating, the extent and shape of the three dimensional region of separated flow ahead of controls on swept wings. (Author).

Technical Abstract Bulletin

DOWNLOAD
Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1961-10

Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961-10 with Military art and science categories.

Index To Nasa Technical Publications

DOWNLOAD
Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.

Scientific And Technical Aerospace Reports

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1994

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.