Comparison of integral and finite-difference methods for predicting the turbulent boundary layer on axisymmetric bodies

An investigation of turbulent flow problems using finite element methods

Hughes, T.G

January 1978

SIGLEAvailable from British Library Document Supply Centre- DSC:DX76490 / BLDSC - British Library Do...

Turbulent boundary layer flow over undulating surfaces

Belcher, S.E

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D60148 / BLDSC - British Library Doc...

Three-dimensional separated flow prediction on fusiform body using Euler and boundary layer methods

Kwong, C-M

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D86846 / BLDSC - British Library Doc...

Comparison of integral and finite-difference methods for predicting the turbulent boundary layer on axisymmetric bodies

Atkins, D.J
Admiralty Marine Technology Establishment, Poole (United Kingdom)

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:2265.63F(BR--108415)(microfiche) / B...

Comparison of measured and computed boundary layers at the tail-end of an axisymmetric body in an air-jet

Cooper, G.J.
Admiralty Marine Technology Establishment, Teddington (UK)

January 1983

SIGLELD:8622.20(AMTE(N)TM--83053) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

The prediction of free turbulent boundary layers by use of a two-equation model of turbulence

Rodi, W

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186773 / BLDSC - British Library D...

Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers /

Bushnell, Dennis M.
Feller, William V.
Harvey, William D.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.Includes bibliographic...

Integral solution of compressible turbulent boundary layers using improved velocity profiles /

Whitfield, David L., author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

A shear-work integral method is developed for calculating compressible turbulent boundary layers on ...

The implementation of a finite difference method for predicting incompressible flows in complex geometries

Burns, A.
Jones, I.
Kightley, J.
UKAEA Atomic Energy Research Establishment, Harwell (United Kingdom). Engineering Sciences Div.
UKAEA Atomic Energy Research Establishment, Harwell (United Kingdom). Computer Science and Systems Div

January 1987

Paper presented at the Fifth Int. Conf. on Numerical Methods in Laminar Turbulent Flow held Montreal...

Experimental verification and comparison of non-intrusive methods for detecting laminar-turbulent transition on a natural laminar flow axisymmetric body

Stewart, I.

January 1997

In 2 vols.Available from British Library Document Supply Centre-DSC:DXN019106 / BLDSC - British Libr...

A turbulent prediction and optimisation method for compressible axisymmetric diffusers

Heravi, M

January 1981

SIGLEAvailable from British Library Document Supply Centre- DSC:D39640/82 / BLDSC - British Library ...

Comparison of surface pressure fluctuations in a turbulent boundary layer as measured on various flight vehicles

Green, A.R
Engineering Sciences Data Unit Ltd. (ESDU), London (United Kingdom)

January 1974

SIGLEAvailable from British Library Lending Division - LD:2265.63F(BR--71686) / BLDSC - British Libr...

Calculation of the boundary-layer flow in the windward symmetry plane of a spherically blunted axisymmetric body at angle of attack, including streamline-swallowing effects /

Mayne, Arloe W., Jr., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Three-dimensional compressible boundary-layer equations are particularized to the windward symmetry ...

Finite-Difference Solution for Laminar or Turbulent Boundary Layer Flow over Axisymmetric Bodies with Ideal Gas, CF4, or Equilibrium Air Chemistry

Greendyke, Robert B.
Millman, Daniel R.
Hamilton, H. Harris, II

December 1992

A computer code was developed that uses an implicit finite-difference technique to solve nonsimilar,...

Calculation and measurement of separated turbulent boundary layers

Smith, P.D.
Hastings, R.C.
Williams, B.R.
Royal Aircraft Establishment, Farnborough (UK)

January 1982

SIGLELD:8670.2(RAE-TM-AERO--1955) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

An investigation of turbulent flow problems using finite element methods

Hughes, T.G

January 1978

SIGLEAvailable from British Library Document Supply Centre- DSC:DX76490 / BLDSC - British Library Do...

Turbulent boundary layer flow over undulating surfaces

Belcher, S.E

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D60148 / BLDSC - British Library Doc...

Three-dimensional separated flow prediction on fusiform body using Euler and boundary layer methods

Kwong, C-M

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D86846 / BLDSC - British Library Doc...

Comparison of integral and finite-difference methods for predicting the turbulent boundary layer on axisymmetric bodies

Atkins, D.J
Admiralty Marine Technology Establishment, Poole (United Kingdom)

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:2265.63F(BR--108415)(microfiche) / B...

Comparison of measured and computed boundary layers at the tail-end of an axisymmetric body in an air-jet

Cooper, G.J.
Admiralty Marine Technology Establishment, Teddington (UK)

January 1983

SIGLELD:8622.20(AMTE(N)TM--83053) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

The prediction of free turbulent boundary layers by use of a two-equation model of turbulence

Rodi, W

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186773 / BLDSC - British Library D...

Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers /

Bushnell, Dennis M.
Feller, William V.
Harvey, William D.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.Includes bibliographic...

Integral solution of compressible turbulent boundary layers using improved velocity profiles /

Whitfield, David L., author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

A shear-work integral method is developed for calculating compressible turbulent boundary layers on ...

The implementation of a finite difference method for predicting incompressible flows in complex geometries

Burns, A.
Jones, I.
Kightley, J.
UKAEA Atomic Energy Research Establishment, Harwell (United Kingdom). Engineering Sciences Div.
UKAEA Atomic Energy Research Establishment, Harwell (United Kingdom). Computer Science and Systems Div

January 1987

Paper presented at the Fifth Int. Conf. on Numerical Methods in Laminar Turbulent Flow held Montreal...

Experimental verification and comparison of non-intrusive methods for detecting laminar-turbulent transition on a natural laminar flow axisymmetric body

Stewart, I.

January 1997

In 2 vols.Available from British Library Document Supply Centre-DSC:DXN019106 / BLDSC - British Libr...

A turbulent prediction and optimisation method for compressible axisymmetric diffusers

Heravi, M

January 1981

SIGLEAvailable from British Library Document Supply Centre- DSC:D39640/82 / BLDSC - British Library ...

Comparison of surface pressure fluctuations in a turbulent boundary layer as measured on various flight vehicles

Green, A.R
Engineering Sciences Data Unit Ltd. (ESDU), London (United Kingdom)

January 1974

SIGLEAvailable from British Library Lending Division - LD:2265.63F(BR--71686) / BLDSC - British Libr...

Calculation of the boundary-layer flow in the windward symmetry plane of a spherically blunted axisymmetric body at angle of attack, including streamline-swallowing effects /

Mayne, Arloe W., Jr., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Three-dimensional compressible boundary-layer equations are particularized to the windward symmetry ...

Finite-Difference Solution for Laminar or Turbulent Boundary Layer Flow over Axisymmetric Bodies with Ideal Gas, CF4, or Equilibrium Air Chemistry

Greendyke, Robert B.
Millman, Daniel R.
Hamilton, H. Harris, II

December 1992

A computer code was developed that uses an implicit finite-difference technique to solve nonsimilar,...

Calculation and measurement of separated turbulent boundary layers

Smith, P.D.
Hastings, R.C.
Williams, B.R.
Royal Aircraft Establishment, Farnborough (UK)

January 1982

SIGLELD:8670.2(RAE-TM-AERO--1955) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

An investigation of turbulent flow problems using finite element methods

Hughes, T.G

January 1978

SIGLEAvailable from British Library Document Supply Centre- DSC:DX76490 / BLDSC - British Library Do...

Turbulent boundary layer flow over undulating surfaces

Belcher, S.E

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D60148 / BLDSC - British Library Doc...

Three-dimensional separated flow prediction on fusiform body using Euler and boundary layer methods

Kwong, C-M

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D86846 / BLDSC - British Library Doc...

Comparison of integral and finite-difference methods for predicting the turbulent boundary layer on axisymmetric bodies

Abstract

Extracted data

Comparison of integral and finite-difference methods for predicting the turbulent boundary layer on axisymmetric bodies

Abstract

Extracted data

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