Pressure Recovery

14 books
New methods of pressure recovery in a supersonic wind tunnelAshton M. Patterson

New methods of pressure recovery in a supersonic wind tunnel

Ashton M. Patterson

1950No page data
IPAC--Inlet Performance Analysis CodePaul J. Barnhart

IPAC--Inlet Performance Analysis Code

Paul J. Barnhart

1997No page data
A computational-experimental development of vortex generator use for a transitioning S-diffuserBruce J. Wendt

A computational-experimental development of vortex generator use for a transitioning S-diffuser

Bruce J. Wendt

1996No page data
Secondary recovery and pressure maintenance operations in Kansas, 1965Robert L. Dilts
⏱ 1h 3m

Secondary recovery and pressure maintenance operations in Kansas, 1965

Robert L. Dilts

196663 pp.
Secondary recovery and pressure maintenance operations in Kansas, 1967Robert L. Dilts
⏱ 1h 11m

Secondary recovery and pressure maintenance operations in Kansas, 1967

Robert L. Dilts

196871 pp.
Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impellerLawrence F. Schumann

Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller

Lawrence F. Schumann

1986No page data
Some observations on transitory stall in conical diffusersK. B. M. Q. Zaman

Some observations on transitory stall in conical diffusers

K. B. M. Q. Zaman

1989No page data
Secondary recovery and pressure maintenance operations in Kansas 1966Robert L. Dilts
⏱ 1h 8m

Secondary recovery and pressure maintenance operations in Kansas 1966

Robert L. Dilts

196768 pp.
Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inletsBernhard H. Anderson

Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets

Bernhard H. Anderson

2002No page data
Wind tunnel pressurization and recovery systemUnknown Author

Wind tunnel pressurization and recovery system

Unknown Author

1988No page data
Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attackKevin R. Walsh

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack

Kevin R. Walsh

1997No page data
Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attackUnknown Author

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack

Unknown Author

1997No page data
Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnelP. S. Barna

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

P. S. Barna

1995No page data
Solar technologies for buildingsUrsula Eicker
⏱ 5h 30m

Solar technologies for buildings

Ursula Eicker

2003330 pp.