Engine Inlets

87 books
Application of CFD to the analysis and design of high-speed inletsWilliam C. Rose

Application of CFD to the analysis and design of high-speed inlets

William C. Rose

1995No page data
Advanced seal technology role in meeting next generation turbine engine goalsBruce M. Steinetz

Advanced seal technology role in meeting next generation turbine engine goals

Bruce M. Steinetz

1998No page data
A numerical analysis applied to high angle of attack three-dimensional inletsDanny P. Hwang

A numerical analysis applied to high angle of attack three-dimensional inlets

Danny P. Hwang

1986No page data
Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attackCrawford F. Smith

Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

Crawford F. Smith

1995No page data
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92Richard J. Re

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

Richard J. Re

1996No page data
Inlet flow test calibration for a small axial compressor rigD. P. Miller

Inlet flow test calibration for a small axial compressor rig

D. P. Miller

1995No page data
Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inletUnknown Author

Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet

Unknown Author

2001No page data
Minimum weight design of a generic axisymmetric inletShari-Beth Nadell

Minimum weight design of a generic axisymmetric inlet

Shari-Beth Nadell

1996No page data
Mach 10 computational study of a three-dimensional scramjet inlet flow fieldScott Douglas Holland

Mach 10 computational study of a three-dimensional scramjet inlet flow field

Scott Douglas Holland

1995No page data
Improved finite element modeling of the turbofan engine inlet radiation problemIndranil Danda Roy

Improved finite element modeling of the turbofan engine inlet radiation problem

Indranil Danda Roy

1993No page data
Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2Unknown Author

Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2

Unknown Author

1991No page data
Inlet flowfield investigationUnknown Author

Inlet flowfield investigation

Unknown Author

1983No page data
Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generatorsSoo-Yong Cho

Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators

Soo-Yong Cho

1994No page data
Fan noise prediction system developmentH. D. Meyer

Fan noise prediction system development

H. D. Meyer

1993No page data
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attackAndrew J. Yuhas

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack

Andrew J. Yuhas

1997No page data
Coastal and inlet processes numerical modeling system for Oregon Inlet, North CarolinaUnknown Author
⏱ 1h 33m

Coastal and inlet processes numerical modeling system for Oregon Inlet, North Carolina

Unknown Author

198593 pp.
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attackUnknown Author

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack

Unknown Author

1997No page data
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attackUnknown Author

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack

Unknown Author

1997No page data
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attackUnknown Author

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack

Unknown Author

1997No page data
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transientsBobby W. Sanders
⏱ 1h 38m

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients

Bobby W. Sanders

198098 pp.
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