Boundary Layer Flow

558 books
Flight Vehicle Aerodynamics. Drela
⏱ 5h 4m

Flight Vehicle Aerodynamics

. Drela

2014304 pp.
Flow of low density air over a heated flat plate at Mach no. 0.5S. A. Gordon

Flow of low density air over a heated flat plate at Mach no. 0.5

S. A. Gordon

1964No page data
Effect of nonzero surface admittance on receptivity and stability of compressible boundary layerMeelan Choudhari

Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer

Meelan Choudhari

1994No page data
Laminar boundary layersLouis Rosenhead
⏱ 11h 27m

Laminar boundary layers

Louis Rosenhead

1963687 pp.
Distributed-roughness effects on stability and transition in swept-wing boundary layersRuben B. Carrillo

Distributed-roughness effects on stability and transition in swept-wing boundary layers

Ruben B. Carrillo

1997No page data
Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3J. E. Bardina

Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3

J. E. Bardina

1994No page data
Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction systemDal V. Maddalon
⏱ 38m

Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system

Dal V. Maddalon

199038 pp.
Computer program for solving laminar, transitional, or turbulent compressible boundary-layer equations for two-dimensional and axisymmetric flowJulius E. Harris
⏱ 2h 24m

Computer program for solving laminar, transitional, or turbulent compressible boundary-layer equations for two-dimensional and axisymmetric flow

Julius E. Harris

1982144 pp.
Unsteady three-dimensional marginal separation, including breakdownPeter W. Duck
⏱ 29m

Unsteady three-dimensional marginal separation, including breakdown

Peter W. Duck

199029 pp.
The velocity field created by a shallow bump in a boundary layerMichael Gaster

The velocity field created by a shallow bump in a boundary layer

Michael Gaster

1994No page data
Interacting boundary-layer solutions for laminar separated flow past airfoilsO. R Burggraf

Interacting boundary-layer solutions for laminar separated flow past airfoils

O. R Burggraf

1984No page data
Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnelJ. Ruptash
⏱ 23m

Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel

J. Ruptash

195223 pp.
A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layersZ. Yang

A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers

Z. Yang

1992No page data
Progress in Favré-Reynolds stress closures for compressible flowsV. Adumitroaie

Progress in Favré-Reynolds stress closures for compressible flows

V. Adumitroaie

1998No page data
Embedded function methods for compressible high speed turbulent flowJ. D. A. Walker

Embedded function methods for compressible high speed turbulent flow

J. D. A. Walker

1994No page data
Notes on Numerical Fluid Mechanics, vol. 86: Recent results in laminar-turbulent transition: selected numerical and experimental contributions from the DFG priority programme 'Transition' in GermanySiegfried Wagner
⏱ 5h 24m

Notes on Numerical Fluid Mechanics, vol. 86: Recent results in laminar-turbulent transition: selected numerical and experimental contributions from the DFG priority programme 'Transition' in Germany

Siegfried Wagner

2003324 pp.
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselagesVenkit Iyer

Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages

Venkit Iyer

1990No page data
Non-linear boundary-layer receptivity due to distributed surface roughnessGregory V. Selby

Non-linear boundary-layer receptivity due to distributed surface roughness

Gregory V. Selby

1995No page data
Numerical boundary condition proceduresSymposium on Numerical Boundary Condition Procedures (1981 NASA Ames Research Center)
⏱ 7h 24m

Numerical boundary condition procedures

Symposium on Numerical Boundary Condition Procedures (1981 NASA Ames Research Center)

1982444 pp.
Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suctionUnknown Author
⏱ 47m

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction

Unknown Author

198347 pp.
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