Investigation of a Thick Laminar Boundary Layer in a Supersonic Nozzle PDF Download
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Author: Donald Eckhart Emerson
Publisher:
ISBN:
Category : Ultrasonic waves
Languages : en
Pages : 246
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Book Description
Author: Donald Eckhart Emerson
Publisher:
ISBN:
Category : Ultrasonic waves
Languages : en
Pages : 246
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Author: Edwin Snow Gallacher
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 214
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Author: Klaus Oswatitsch
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Book Description
Summary: The present report consists of two parts. The first part deals with the two-dimensional stationary flow in the presence of local supersonic zones. A numerical method of integration of the equation of gas dynamics is developed. Proceeding from solutions at great distance from the body the flow pattern is calculated step by step. Accordingly the related body form is obtained at the end of the calculation. The second part treats the relationship between the displacement thickness of laminar and turbulent boundary layers and the pressure distribution at high speeds. The stability of the boundary layer is investigated, resulting in basic differences in the behavior of subsonic and supersonic flows. Lastly, the decisive importance of the boundary layer for the pressure distribution, particularly for thin profiles, is demonstrated.
Author: J. P. Kreskovsky
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 100
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Author: Laura L. Pauley
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: William D. Harvey
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92
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Author: Robert L. P. Voisinet
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 144
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The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract).
Author: S. William Gouse
Publisher:
ISBN:
Category :
Languages : en
Pages : 286
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Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 580
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Author: John Russell Radbill
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 216
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