Start Over
You searched for: author_facet Anderson, Bernhard H.

Search Results

Cover image for Experimental investigation of the application of microramp flow control to an oblique shock interaction

Experimental investigation of the application of microramp flow control to an oblique shock interaction

Location
Access Content Online
Cover image for Design-of-experiments to reduce life-cycle costs in combat aircraft inlets

Design-of-experiments to reduce life-cycle costs in combat aircraft inlets

Location
Access Content Online
Cover image for Design-of-experiments to reduce life-cycle costs in combat aircraft inlets

Design-of-experiments to reduce life-cycle costs in combat aircraft inlets

Location Call # Status
Joyner - Microforms B300 NAS 1.15:2003-212017 ✔ Available
Cover image for 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

Location
Access Content Online
Cover image for 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

Location Call # Status
Joyner - Microforms B300 NAS 1.15:2002-212000 ✔ Available
Cover image for A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers

A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers

Location Call # Status
Joyner - Microforms B300 NAS 1.15:211278 ✔ Available
Cover image for Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Location Call # Status
Joyner - Microforms B300 NAS 1.15:106580 ✔ Available
Cover image for The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct

The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct

Location Call # Status
Joyner - Microforms B300 NAS 1.15:103703 ✔ Available
Cover image for A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics

A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics

Location Call # Status
Joyner - Microforms B300 NAS 1.15:104436 ✔ Available
Cover image for Internal fluid mechanics research on supercomputers for aerospace propulsion systems

Internal fluid mechanics research on supercomputers for aerospace propulsion systems

Location Call # Status
Joyner - Microforms B300 NAS 1.15:100289 ✔ Available