Proceedings of Low-Speed Boundary-Layer Transition Workshop

II
  • 287 Pages
  • 2.34 MB
  • 5715 Downloads
  • English
by , Santa Monica , Calif. : Rand Corp., 1978
StatementWilliam S. King, Mari Yokota.
SeriesRand paper series ; P-6119
Classifications
LC ClassificationsMLCM 83/4498 (T)
The Physical Object
Paginationix, 287 p. : ill. ; 29 cm.
ID Numbers
Open LibraryOL4441465M
LC Control Number79102933

Low-speed Boundary-layer Transition Workshop (2nd: Santa Monica, Calif.). Proceedings of [the] Low-speed Boundary-layer Transition Workshop: II. Santa Monica: Rand Corporation, (OCoLC) Material Type: Conference publication: Document Type: Book: All Authors / Contributors: William S King; Mari Yokota; Rand Corporation.

"This report has been prepared to document the Low-Speed Boundary-Layer Transition Workshop held at the offices of the Rand Corporation July"--Preface. "A report prepared for Defense Advanced Research Projects Agency and Office of Naval Research.".

Hama and J. Nutant, “ Detailed flow-field observations in the transition process in a thick boundary layer,” in Proceedings of the Heat Transfer and Fluid Mechanics Institute (Stanford University Press, ), pp.

77– found experimentally that a special structure, called a kink, appeared before the Λ-vortex during the process of. 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, Gad-el-Hak, M.

(editor) () Proceedings of the U.S.{Egypt Workshop on Predictive Methodologies for Global Weather-Related Disasters, CD Publication, Virginia Commonwealth University, Richmond, Virginia. Gad-el-Hak, M. (editor) () Proceedings of.

Flow measurements were made on a highly loaded low pressure turbine blade in a low-speed linear cascade facility. The blade has a design Zweifel coefficient of with a peak pressure coefficient near 47% axial chord (midloaded).Cited by: 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, The work­ shop coincided with the initiation of Proceedings of Low-Speed Boundary-Layer Transition Workshop book.

Power, L.: A Comparison Between Measured and Computed Locations of Transition on Nine Forebodies of Revolution. Proceedings of Low-Speed Boundary Layer Transition Workshop, II, Rand Corporation Report R-P, (Eds.: W.

King and M.

Details Proceedings of Low-Speed Boundary-Layer Transition Workshop FB2

Yokota). Google ScholarCited by: Stanford Libraries' official online search tool for books, media, journals, databases, government documents and more.

The basic problems of transition in both incompressible and compressible boundary layers are reviewed. Flow structures in low-speed transitional and developed turbulent boundary layers are presented, together with almost all of the physical mechanisms that have been proposed for.

The analysis is based on the combination of the shear stress transport turbulence model with the γ - R ˜ e θ t transition model, which can handle the laminar boundary layer and its transition. Full text of "Minnowbrook II Workshop on Boundary Layer Transition in Turbomachines" See other formats.

Transition in oscillating boundary layer flow, Journal of Fluid Mechan 93– Obremski, H. and Morkovin, M. Application of a quasi-steady stability model to periodic boundary layer flows, AIAA Journal 7, –Cited by: This page in the original is blank.

A fully elliptic numerical method for the solution of the Reynolds Averaged Navier Stokes Equations is applied to the flow around the HSVA Tanker. The weaknesses of the simulation are analysed by comparing several discretisation schemes and grids as well as.

Description Proceedings of Low-Speed Boundary-Layer Transition Workshop PDF

The U2 profile was designed to meet the targets of reduced cost, weight and fuel burn of aircraft engines. The studies were conducted on both low-speed and high-speed experimental facilities under the unsteady flow conditions with upstream passing wakes. The current paper presents the low-speed investigation results.

Proceedings 14th CEAS-ASC Workshop and 5th Scientific Workshop of X3-Noise. 14th Council of European Aerospace boundary layer transition detection, skin friction drag 15 Experimental study of an ECCOMAS proceedings e-book J. Eberhardsteiner Vienna (Austria) Abstract Issues related to prediction of laminar-turbulent transition on hypersonic configurations in high-altitude flight are discussed.

The laminar flow control strategy and appropriate laminarization methods for high-speed vehicles are reviewed. The paper is aimed to motivate the transition study groups to integrate their knowledge and tools in the rational framework of the amplitude by: The effects of convex curvature on boundary layer transition were examined experimentally in low and high free-stream turbulence, and in zero and favorable pressure gradients.

For high turbulence with zero pressure gradient, transition along convex surfaces was found to be similar to that on flat surfaces, however at low turbulence levels.

Proceedings of the 5th ERCOFTAC workshop "Direct and Large-Eddy Simulation 5" (DLES-5), held at Munich University of Technology, AugustISBN (alk.

paper) (hbk.: alk. paper) (e-book) (e-book). The proceedings of the third Workshop on Change of representation and Problem Reformulation is presented. In contrast to the first two workshops, this workshop was focused on analytic or knowledge-based approaches, as opposed to statistical or empirical approaches called 'constructive induction'.

Workshop on Boundary Layer Transition. Walker, G., " Transition in Turbomachines-An Overview, " Proceedings of Minnowbrook II Workshop on Boundary Layer Transition in Turbomachines, NASA/CP.

Full text of "Proceedings of the Workshop on Flow in Turbomachines" See other formats. In the interest of being able to predict separating–reattaching flows, it is necessary to have an accurate model of transition in separation bubbles.

An experimental investigation of the process of turbulence development in a separation bubble shows that transition occurs within the separated shear by: The equation of continuity and the stream-surface equation will now be applied to generalize the thin boundary-layer treatments of Moore [] and Lighthill [] for a double ship (x,y,z) denote a rectangular Cartesian coordinate system with origin at the forward stagnation point, the x-axis parallel to the uniform stream and positive in the downstream direction, with the x- and z-axes.

Fasel, H. F., Gross, A., and Postl D., “Numerical Simulation of Active Flow Control for Low Pressure Turbine Blades,” NATA Research & Technology Organization Applied Vehicle Technology Panel Specialist Meeting on “Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation.

Schneider, Steven P. Flight data for boundary-layer transition at hypersonic and supersonic speeds. Journal of spacecraft and rockets, v.

36, Jan./Feb. Weis-Fogh, Torkel. Energetics and aerodynamics of flapping flight: a synthesis. In Insect flight. Edited on.

This document contains the proceedings of the Training Workshop on Nondeterministic Approaches and Their Potential for Future Aerospace Systems held at NASA Langley Research Center, Hampton, Virginia, May 1, Results of the Scale Shuttle Orbiter Vehicle Boundary Layer Transition Wind Tunnel Test (MH) in the AEDC VKF.

Proceedings of IUTAM Symposia and Summer Schools. Fromif the organizers of a Symposium decide to publish proceedings, the recommended form of publication is the IUTAM Bookseries by Springer. From toProcedia IUTAM by Elsevier was the preferred medium of publication for the refereed proceedings of IUTAM symposia.

It is open January until December.

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This book constitutes the refereed proceedings of the 15th International Conference on Automated Deduction, CADE, held in Lindau, Germany, in July The volume presents three invited contributions together with 25 revised full papers and 10 revised system descriptions; these were Author: Charles-Henri Bruneau.

This book is primarily intended as a graduate level text in turbulent flows for engineering students, but it may also be valuable to students in applied mathematics, physics, oceanography and atmospheric sciences, as well as researchers and practising : Stephen B.

Pope. Detection of Boundary Layer Transition in High and Low Speed Wind Tunnels at the Institute for Aerospace Research''", First Bombardier International Workshop, Montreal, Quebec.First of all the results of the 2-C-multiplane PIV measurements will be presented to give an overview of the whole spot structure.

The x-axis is directed stream-wise, the y-axis wall-normal and the z-axis span-wise, the corresponding velocity components are u, v and instantaneous velocity vector fields of the same spot at a wall distance of y = mm and with a time-separation of t = 5 Cited by: 1.Whitfield, D.

L., "Turbulent Flow Near a Wall Based on a Turbulent Kinetic Energy Equation," in Boundary Layer Effects-Proceedings of the 5th U.S. Air Force-Federal Republic of Germany Data Exchange Agreement Meeting, A.W.

Fiore, Editor, AFFDL-TR, Julypp.