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Effect Of Bluntness And Angle Of Attack On Boundary Layer Transition On Cones And Biconic Configurations
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Book Synopsis Effect of Bluntness and Angle of Attack on Boundary Layer Transition on Cones and Biconic Configurations by : Kenneth F. Stetson
Download or read book Effect of Bluntness and Angle of Attack on Boundary Layer Transition on Cones and Biconic Configurations written by Kenneth F. Stetson and published by . This book was released on 1978 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Correlation of Artifically Induced Boundary-layer Transition Data from Blunt Slender Cones at Hypersonic Speeds by : Albert H. Boudreau
Download or read book A Correlation of Artifically Induced Boundary-layer Transition Data from Blunt Slender Cones at Hypersonic Speeds written by Albert H. Boudreau and published by . This book was released on 1979 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1989 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1989 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack by :
Download or read book Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack written by and published by . This book was released on 1986 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of nosetip bluntness on cone frustrum boundary layer transition were investigated by conducting hypersonic wind tunnel experiments. Frustrum transition Reynolds numbers were found to have large variations within the entropy layer swallowing region. Investigation results indicated that several nosetip blunting effects were competing for the dominant role in the frustrum transition process and it was speculated that the large variations in transition Reynolds number were associated with the shifting of dominant roles. Based upon these studies, dominant nosetip bluntness effects are tentatively identified with three regions of the entropy layer. Transition movement and patterns on the frustrum of a cone at small angles of attack were investigated at a Mach number of 5.9, using an 8-deg half angle cone with both sharp and blunt nosetips. Small angles of attack produced large asymmetries in the frustrum transition pattern for both sharp and blunt tipped configurations. For the configurations with nosetip bluntness most of the frustrum transition asymmetry occurred between meridian angles of 60 and 120 deg. Data obtained with simulated laminar ablated nosetips were generally representative of what would be expected with a larger spherically blunt nosetip. Keywords: Boundary layer transition; Angle of attack.
Book Synopsis The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 1 by : Sangchul Lee
Download or read book The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 1 written by Sangchul Lee and published by Springer Nature. This book was released on 2022-08-30 with total page 1027 pages. Available in PDF, EPUB and Kindle. Book excerpt: This proceeding comprises peer-reviewed papers of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), held from 15-17 November 2021 in Jeju, South Korea. This book deals with various themes on computational fluid dynamics, wind tunnel testing, flow visualization, UAV design, flight simulation, satellite attitude control, aeroelasticity and control, combustion analysis, fuel injection, cooling systems, spacecraft propulsion and so forth. So, this book can be very helpful not only for the researchers of universities and academic institutes, but also for the industry engineers who are interested in the current and future advanced topics in aerospace technology.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range by : J. Leith Potter
Download or read book Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range written by J. Leith Potter and published by . This book was released on 1975 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The feasibility of determining Reynolds numbers of boundary layer transition on sharp, 10-deg, semiangle cones at slightly supersonic free-stream Mach numbers, 1.04 = or
Book Synopsis Boundary-Layer Transition on Blunt, Slender Cones at Hypersonic Mach Numbers by : Kenneth F. Stetson
Download or read book Boundary-Layer Transition on Blunt, Slender Cones at Hypersonic Mach Numbers written by Kenneth F. Stetson and published by . This book was released on 1982 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: New wind tunnel data has been obtained to investigate the effects of tip bluntness and angle of attack on boundary layer transition on slender cones. The rearward displacement of transition due to tip bluntness and the maximum displacement of transition are reasonably well understood and explainable primarily on the basis of a reduction in local Reynolds number due to pressure losses across the bow shock. The rapid forward movement of transition observed on the cone frustum is a mystery and will be studied further in future experiments. The observed rapid movement of transition from the sphere-cone tangency point to the subsonic region of the tip is compatible with stability analysis and has been observed by several experimentalists. The transition movements obtained on the sharp cone at angle of attack were compatible with both theory and other experiments. The movements of transition on blunt cones at angle of attack remains poorly understood. The present results appear reasonable; however, since many different trends have been observed in transition experiments and since there is little guidance available from stability analyses, additional confirmation of these transition trends are needed. (Author).
Book Synopsis A Review of High-speed, Convective, Heat-transfer Computation Methods by : Michael E. Tauber
Download or read book A Review of High-speed, Convective, Heat-transfer Computation Methods written by Michael E. Tauber and published by . This book was released on 1989 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 by : Michael C. Fischer
Download or read book An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 written by Michael C. Fischer and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Boundary layer transition on nose cones at hypersonic speeds.
Book Synopsis Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M[mathematical Symbol for Infinity] by : George G. Mateer
Download or read book Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M[mathematical Symbol for Infinity] written by George G. Mateer and published by . This book was released on 1972 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted on 5 deg and 15 deg half-angle sharp cones at wall-to-total-temperature ratios of 0.08 to 0.4, and angles of attack from 0 deg to 20 deg. The results indicate that (1) transition Reynolds numbers decrease with decreasing temperature ratio, (2) local transition Reynolds numbers decrease from the windward to the leeward side of the model, and (3) transition data on the windward ray of cones can be correlated in terms of the crossflow velocity gradient, momentum thickness Reynolds number, local Mach number, and cone half-angle.
Book Synopsis Hypersonic Boundary Layer Transition Experiments by : Kenneth F. Stetson
Download or read book Hypersonic Boundary Layer Transition Experiments written by Kenneth F. Stetson and published by . This book was released on 1980 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Tip Bluntness on Boundary-layer Transition on a 15 Degrees Included Angle Cone at M by : Ruth H. Rogers
Download or read book The Effect of Tip Bluntness on Boundary-layer Transition on a 15 Degrees Included Angle Cone at M written by Ruth H. Rogers and published by . This book was released on 1959 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects by : Arloe Wesley Mayne (Jr.)
Download or read book Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects written by Arloe Wesley Mayne (Jr.) and published by . This book was released on 1972 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1981 with total page 1060 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis In-flight Transition Measurement on a 100 Cone at Mach Numbers from 0.5 to 2.0 by : David F. Fisher
Download or read book In-flight Transition Measurement on a 100 Cone at Mach Numbers from 0.5 to 2.0 written by David F. Fisher and published by . This book was released on 1982 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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