Base Flow Aerodynamics

11 books
The wedge hot-film anemometer in supersonic flowJohn M. Seiner
⏱ 54m

The wedge hot-film anemometer in supersonic flow

John M. Seiner

198354 pp.
Aerodynamics of base combustionWorkshop on Aerodynamics of Base Combustion Purdue University 1974.
⏱ 8h 42m

Aerodynamics of base combustion

Workshop on Aerodynamics of Base Combustion Purdue University 1974.

1976522 pp.
Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughnessStephen A. Whitmore

Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness

Stephen A. Whitmore

2001No page data
Approximate indicial lift function for tapered, swept wings in incompressible flowM. J. Queijo
⏱ 29m

Approximate indicial lift function for tapered, swept wings in incompressible flow

M. J. Queijo

197829 pp.
Accelerated convergence for incompressible flow calculationsG. M Neely

Accelerated convergence for incompressible flow calculations

G. M Neely

1985No page data
On the upstream influence of the base pressureRobert F. Weiss
⏱ 23m

On the upstream influence of the base pressure

Robert F. Weiss

196723 pp.
Nonlinear interaction between a pair of oblique modes in a supersonic mixing layerThomas F. Balsa

Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer

Thomas F. Balsa

1995No page data
Approximate indicial lift function for tapered, swept wings in incompressible flowM. J Queijo
⏱ 29m

Approximate indicial lift function for tapered, swept wings in incompressible flow

M. J Queijo

197829 pp.
The wedge hot-film anemometer in supersonic flowJohn M Seiner
⏱ 54m

The wedge hot-film anemometer in supersonic flow

John M Seiner

198354 pp.
The wedge hot-film anemometer in supersonic flowJohn M Seiner
⏱ 54m

The wedge hot-film anemometer in supersonic flow

John M Seiner

198354 pp.
Lobed mixer design for noise suppressionVinod Govind Mengle

Lobed mixer design for noise suppression

Vinod Govind Mengle

2002No page data