Subsonic Flow

90 books
Application of linearized transonic theory to tunnel blockage interferenceC. F. Lo
⏱ 28m

Application of linearized transonic theory to tunnel blockage interference

C. F. Lo

197428 pp.
The Kirchhoff formulas for moving surfaces in aeroacousticsF. Farassat

The Kirchhoff formulas for moving surfaces in aeroacoustics

F. Farassat

1996No page data
Determination of the pressure drag of airfoils by integration of surface pressuresWilliam H. Phillips

Determination of the pressure drag of airfoils by integration of surface pressures

William H. Phillips

1990No page data
Doppler global velocimetry at NASA Glenn Research CenterChristian T. Lant

Doppler global velocimetry at NASA Glenn Research Center

Christian T. Lant

2003No page data
Acoustic and laser doppler anemometer results for confluent and 120-lobed E³ mixer exhaust systems for subsonic jet noise reductionUnknown Author

Acoustic and laser doppler anemometer results for confluent and 120-lobed E³ mixer exhaust systems for subsonic jet noise reduction

Unknown Author

2002No page data
Study of the unsteady flow features on a stalled wingS. Yon

Study of the unsteady flow features on a stalled wing

S. Yon

1997No page data
The role of freestream turbulence scale in subsonic flow separationUnknown Author

The role of freestream turbulence scale in subsonic flow separation

Unknown Author

1985No page data
Shock tunnel studies of scramjet phenomena 1994R. G. Morgan

Shock tunnel studies of scramjet phenomena 1994

R. G. Morgan

1997No page data
Shock tunnel studies of scramjet phenomena 1995R. G. Morgan

Shock tunnel studies of scramjet phenomena 1995

R. G. Morgan

1997No page data
Application of chimera grid scheme to combustor flowfields at all speedsShaye Yungster

Application of chimera grid scheme to combustor flowfields at all speeds

Shaye Yungster

1997No page data
A numerical simulator for three-dimensional flows through vibrating blade rowsH. Andrew Chuang

A numerical simulator for three-dimensional flows through vibrating blade rows

H. Andrew Chuang

1998No page data
Axis switching and spreading of an asymmetric jetK. B. M. O. Zaman

Axis switching and spreading of an asymmetric jet

K. B. M. O. Zaman

1994No page data
Correction for wall-interference by means of a measured-boundary-conditon methodTh. E. Labrujere
⏱ 41m

Correction for wall-interference by means of a measured-boundary-conditon method

Th. E. Labrujere

198441 pp.
Application of the pressure sensitive paint technique to steady and unsteady flowY. Shimbo

Application of the pressure sensitive paint technique to steady and unsteady flow

Y. Shimbo

1996No page data
Role of boundary conditions in Monte Carlo simulation of MEMS devicesRobert P. Nance

Role of boundary conditions in Monte Carlo simulation of MEMS devices

Robert P. Nance

1997No page data
Computational investigations of noise suppression in subsonic round jetsC. David Pruett

Computational investigations of noise suppression in subsonic round jets

C. David Pruett

1997No page data
Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3DS. Paul Pao

Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D

S. Paul Pao

1996No page data
A transonic model representation for two-dimensional wall interference assessmentJ. Smith
⏱ 20m

A transonic model representation for two-dimensional wall interference assessment

J. Smith

198620 pp.
TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurationsUnknown Author

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

Unknown Author

1992No page data
TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurationsUnknown Author

TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations

Unknown Author

1992No page data
← PreviousPage 2 of 5Next →