1
Dan Miller
Philip P Truax, Daniel N Miller, Jeffrey W Hamstra, Patrick J Yagle: System and method for actively manipulating and controlling fluid flow over a surface. Lockheed Martin Corporation, Koestner Bertani, January 27, 2004: US06682021 (17 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic fluid flow over a surface. More specifically, the present invention provides a system and method to control aerodynamic or hydrodynamic fluid flow behavior of a ducted fluid flow ...


2
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Lockheed Martin Corporation, Bracewell & Giuliani, March 31, 2009: US07510149 (11 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


3
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Lockheed Martin Corporation, Bracewell & Giuliani, October 18, 2011: US08038102 (6 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


4
Dan Miller
Philip P Truax, Daniel N Miller, Edward C Ma: Flow control redistribution to mitigate high cycle fatigue. Lockheed Martin Corporation, Bracewell & Giuliani, March 26, 2013: US08402738 (1 worldwide citation)

A method operable to improve pressure recovery and/or distortion within engine inlet is disclosed. A first fluid flow is provided to primary jet vortex generator(s) operable to inject fluid at a first injection rate into a boundary layer of a primary fluid flow within the inlet. A secondary fluid fl ...


5
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Koestner Bertani, February 2, 2006: US20060022092-A1

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


6
Dan Miller
Daniel N Miller, Philip P Truax, Patrick J Yagle: System and method to control flowfield vortices with micro-jet arrays. Bracewell & Giuliani, April 8, 2010: US20100084514-A1

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic flow field vortices within a fluid flow over a surface using micro-jet arrays. The system and method for actively manipulating and controlling the inception point, size and trajec ...


7
Dan Miller
Philip P Truax, Daniel N Miller, Edward C Ma: Flow control redistribution to mitigate high cycle fatigue. Bracewell & Giuliani, January 7, 2010: US20100003129-A1

The present invention provides a method operable to improve pressure recovery and/or distortion within engine inlet. This method involves providing a first fluid flow to primary jet vortex generator(s) operable to inject fluid at a first injection rate into a boundary layer of a primary fluid flow w ...


8
Philip P Truax, Daniel N Miller, Jeffrey W Hamstra, Patrick J Yagle: System and method for manipulating and controlling fluid flow over a surface. Lockheed Martin Corporation, William N Hulsey III, Hughes & Luce L, April 16, 2002: US06371414 (23 worldwide citation)

The present invention provides a system and method for actively manipulating and controlling aerodynamic or hydrodynamic fluid flow over a surface. More specifically, the present invention provides a system and method to control aerodynamic or hydrodynamic fluid flow behavior of a ducted fluid flow ...


9
Philip P Truax, Daniel N Miller, Edward C Ma: Flow control redistribution to mitigate high cycle fatigue. Lockheed Martin Corporation, Bracewell & Giuliani, November 17, 2009: US07617670 (20 worldwide citation)

A method operable to improve pressure recovery and/or distortion within engine inlet is disclosed. A first fluid flow is provided to primary jet vortex generator(s) operable to inject fluid at a first injection rate into a boundary layer of a primary fluid flow within the inlet. A secondary fluid fl ...


10
Philip P Truax: Flow control redistribution to mitigate high cycle fatigue. Lockheed Martin Corporation, ROBERT A McLAUCHLAN, October 4, 2007: US20070227153-A1

The present invention provides a method operable to improve pressure recovery and/or distortion within engine inlet. This method involves providing a first fluid flow to primary jet vortex generator(s) operable to inject fluid at a first injection rate into a boundary layer of a primary fluid flow w ...



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