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Neal E Hass

from Yorktown, VA
Age ~57
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Also known as:
Neal Etal Hass, Neal Teresa Hass, Neal T Hass, Neale Hass, Edward Hass Neal
Phone and address:
113 Swanson Ct, Yorktown, VA 23693
(757) 234-4404
Related to:
William Robert Martin, 86Audrey Martin, 68Joseph Miller, 52Tina Martin, 65
Connected to:
Ana Hass, 61Anne L Hass, 103Ashley Hass, 41Bartley C Hass, 47Brad F Hass, 37Bruce A Hass, 63Chelsey S Hass, 29Christopher E Hass, 47Cory S Hass, 33Craig J Hass, 46

Neal Hass Phones & Addresses

  • 113 Swanson Ct, Yorktown, VA 23693 (757) 234-4404
  • 200 Cybernetics Way, Yorktown, VA 23693
  • 43441 Grange St, Lancaster, CA 93535 (661) 723-1721
  • Lansing, NY
  • Potsdam, NY
  • Los Angeles, CA

Work

Company: Nasa langley research center Jun 2003 Position: Aerospace propulsion engineer

Education

School / High School: Clarkson University 1985 to 1991

Industries

Aviation & Aerospace

Resumes

Resumes

Neal Hass Photo 1

Aerospace Propulsion Engineer At Nasa Langley Research Center

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Position:
Aerospace Propulsion Engineer at NASA Langley Research Center, Aerospace Propulsion Engineer at NASA
Location:
Norfolk, Virginia Area
Industry:
Aviation & Aerospace
Work:
NASA Langley Research Center since Jun 2003
Aerospace Propulsion Engineer
NASA since 1998
Aerospace Propulsion Engineer
NASA Dryden Flt Research Ctr Mar 1997 - Jun 2003
Aerospace Engineer
Education:
Clarkson University 1985 - 1991

Publications

Us Patents

Method Of Simulating Flow-Through Area Of A Pressure Regulator

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US Patent:
20090287460, Nov 19, 2009
Filed:
Jul 7, 2005
Appl. No.:
11/177664
Inventors:
Neal E. Hass - Yorktown VA, US
Paul A. Schallhorn - Indialantic FL, US
Assignee:
USA as represented by the Administrator of the National Aeronautics and Space Administration - Washington DC
International Classification:
G06F 17/10
G06G 7/48
US Classification:
703 2, 703 9
Abstract:
The flow-through area of a pressure regulator positioned in a branch of a simulated fluid flow network is generated. A target pressure is defined downstream of the pressure regulator. A projected flow-through area is generated as a non-linear function of (i) target pressure, (ii) flow-through area of the pressure regulator for a current time step and a previous time step, and (iii) pressure at the downstream location for the current time step and previous time step. A simulated flow-through area for the next time step is generated as a sum of (i) flow-through area for the current time step, and (ii) a difference between the projected flow-through area and the flow-through area for the current time step multiplied by a user-defined rate control parameter. These steps are repeated for a sequence of time steps until the pressure at the downstream location is approximately equal to the target pressure.
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Neal E Hass from Yorktown, VA, age ~57 Get Report