Tomeki

Explore Books on
pressure recovery

1-8 of 8 Books

View Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel By P. S. Barna

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

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

By P. S. Barna

View IPAC--Inlet Performance Analysis Code By Paul J. Barnhart

IPAC--Inlet Performance Analysis Code

IPAC--Inlet Performance Analysis Code

By Paul J. Barnhart

View A computational-experimental development of vortex generator use for a transitioning S-diffuser By Bruce J. Wendt

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

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

By Bruce J. Wendt

View Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets By Bernhard H. Anderson

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

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

By Bernhard H. Anderson

View New methods of pressure recovery in a supersonic wind tunnel By Ashton M. Patterson

New methods of pressure recovery in a supersonic wind tunnel

New methods of pressure recovery in a supersonic wind tunnel

By Ashton M. Patterson

View Some observations on transitory stall in conical diffusers By K. B. M. Q. Zaman

Some observations on transitory stall in conical diffusers

Some observations on transitory stall in conical diffusers

By K. B. M. Q. Zaman

View Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller By Lawrence F. Schumann

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

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

By Lawrence F. Schumann

View Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack By Kevin R. Walsh

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

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

By Kevin R. Walsh