Start Over
You searched for: subject "Laminar flow"

Search Results

Cover image for Generation and development of small-amplitude disturbances in a laminar boundary layer in the presence of an acoustic field

Generation and development of small-amplitude disturbances in a laminar boundary layer in the presence of an acoustic field

Joyner Library - Microforms B300
Call Number: NAS 1.15:77826
Cover image for Theory of Laminar flows

Theory of Laminar flows

Joyner Library - General Stacks
Call Number: TL573 .H52 VOL. 4
Cover image for Laminar flow aircraft certification

Laminar flow aircraft certification

  • 1986
  • Format: Microform
Location
Access Content Online
Cover image for Stability of parallel flow

Stability of parallel flow

Joyner Library - General Stacks
Call Number: QC151 .B44
Cover image for Numerical flow visualization in basic- and hyper-cluster spheres

Numerical flow visualization in basic- and hyper-cluster spheres

  • 1997
  • Format: Book
Joyner Library - Microforms B300
Call Number: NAS 1.15:107361
Cover image for The theory of laminar boundary layers in compressible fluids

The theory of laminar boundary layers in compressible fluids

Joyner Library - General Stacks
Call Number: QA913 .S85
Cover image for Laminar boundary layers

Laminar boundary layers

Joyner Library - General Stacks
Call Number: QC151 .R58
Cover image for Numerical simulations of three-dimensional laminar flow over a backward facing step; flow near side walls

Numerical simulations of three-dimensional laminar flow over a backward facing step; flow near side walls

  • 1993
  • Format: Book
Joyner Library - Microforms B300
Call Number: NAS 1.15:106248
Cover image for A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations

A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations

Location
Access Content Online
Cover image for Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

Location
Access Content Online