Experimental Study Of Nozzle Wall Boundary Layers At Mach Numbers 20 To 47

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Experimental Study of Nozzle Wall Boundary Layers at Mach Numbers 20 to 47

Joseph H. Kemp,F. Kevin Owen
Experimental Study of Nozzle Wall Boundary Layers at Mach Numbers 20 to 47 Book PDF

Author : Joseph H. Kemp,F. Kevin Owen
Publisher : Unknown
Page : 116 pages
File Size : 48,5 Mb
Release : 1972
Category : Aerodynamics, Hypersonic
ISBN : UIUC:30112106640813

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Experimental Study of Nozzle Wall Boundary Layers at Mach Numbers 20 to 47 by Joseph H. Kemp,F. Kevin Owen Pdf

The nozzle wall boundary layer of an M-50 helium tunnel was investigated with pitot pressure, total temperature, skin friction, and wall heat transfer measurements at five stations and hot wire measurements at two stations. The results indicated that the boundary layer was turbulent with a thick viscous sublayer. Pressure gradients were observed across the boundary layer; the effect of these gradients on the equations of motion are discussed. The direct skin friction measurements were higher than expected from empirical predictions; the Reynolds analogy factors however were lower than expected. Hot wire measurements indicated mass flow fluctuations as large as 80 percent of the local mean mass flow at the edge of the viscous sublayer with a maximum value relative to the edge mass flow of about 15 percent at gamma about equal to 0.8.

NASA Technical Note

Anonim
NASA Technical Note Book PDF

Author : Anonim
Publisher : Unknown
Page : 460 pages
File Size : 52,7 Mb
Release : 1972
Category : Electronic
ISBN : MINN:31951000846421F

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NASA Technical Note by Anonim Pdf

NASA Technical Paper

Anonim
NASA Technical Paper Book PDF

Author : Anonim
Publisher : Unknown
Page : 90 pages
File Size : 44,6 Mb
Release : 1978
Category : Science
ISBN : STANFORD:36105024755873

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NASA Technical Paper by Anonim Pdf

NASA Technical Paper

United States. National Aeronautics and Space Administration
NASA Technical Paper Book PDF

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 802 pages
File Size : 46,6 Mb
Release : 1978
Category : Aeronautics
ISBN : UOM:39015039955359

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NASA Technical Paper by United States. National Aeronautics and Space Administration Pdf

Applied Mechanics Reviews

Anonim
Applied Mechanics Reviews Book PDF

Author : Anonim
Publisher : Unknown
Page : 592 pages
File Size : 44,5 Mb
Release : 1974
Category : Mechanics, Applied
ISBN : UCAL:C2682446

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Applied Mechanics Reviews by Anonim Pdf

Comparisons of Turbulent-boundary-layer Measurements at Mach Number 19.5 with Theory and an Assessment of Probe Errors

Ivan E. Beckwith,Frank L. Clark,William D. Harvey
Comparisons of Turbulent boundary layer Measurements at Mach Number 19 5 with Theory and an Assessment of Probe Errors Book PDF

Author : Ivan E. Beckwith,Frank L. Clark,William D. Harvey
Publisher : Unknown
Page : 100 pages
File Size : 50,7 Mb
Release : 1971
Category : Heat
ISBN : UIUC:30112106691964

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Comparisons of Turbulent-boundary-layer Measurements at Mach Number 19.5 with Theory and an Assessment of Probe Errors by Ivan E. Beckwith,Frank L. Clark,William D. Harvey Pdf

Measurements of total temperature and pitot pressure across boundary layer of test section wall of axisymmetric contoured nozzle at hypersonic speed in nitrogen.

Research Review

United States. Air Force. Office of Aerospace Research
Research Review Book PDF

Author : United States. Air Force. Office of Aerospace Research
Publisher : Unknown
Page : 138 pages
File Size : 54,7 Mb
Release : 1970
Category : Astronautics
ISBN : OSU:32435059135129

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Research Review by United States. Air Force. Office of Aerospace Research Pdf

Research Review

Anonim
Research Review Book PDF

Author : Anonim
Publisher : Unknown
Page : 324 pages
File Size : 45,8 Mb
Release : 1969
Category : Research
ISBN : IND:30000089317592

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Research Review by Anonim Pdf

Turbulent Shear Layers in Supersonic Flow

Alexander J. Smits,Jean-Paul Dussauge
Turbulent Shear Layers in Supersonic Flow Book PDF

Author : Alexander J. Smits,Jean-Paul Dussauge
Publisher : Springer Science & Business Media
Page : 418 pages
File Size : 40,6 Mb
Release : 2006-05-11
Category : Science
ISBN : 9780387263052

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Turbulent Shear Layers in Supersonic Flow by Alexander J. Smits,Jean-Paul Dussauge Pdf

A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.