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Yueping Guo

from Saipan, MP
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Also known as:
Yu Guo
Related to:
Yuke Gu, 30Yu Guo
Connected to:
Aaron S Guo, 29Aige Guo, 58Amie Guo, 33Angela W Guo, 34Calvin Guo, 29Carolyn Q Guo, 66Charlie J Guo, 27Chengan A Guo, 69Cindy L Guo, 68Da Z Guo, 46

Yueping Guo Phones & Addresses

  • Saipan, MP
  • Rowland Heights, CA
  • Rowland Heights, CA

Education

Degree: Doctorates, Doctor of Philosophy School / High School: University of Cambridge 1983 to 1986 Specialities: Philosophy

Skills

Fortran • Airframe Noise Modeling • Sonic Environment • Aircraft Noise Reduction • Engineering Management • Aerospace Engineering • Ray Tracing • Aeroacoustics • Fluid Mechanics • Fluid Dynamics • Numerical Analysis • Aeroelasticity • Matlab • Aerodynamics • Msc.patran • Unconventional Aircraft Acoustics • Acoustic Fatigue • Boundary Element Method • Engineering • Wind Tunnel Testing • Finite Element Analysis • Computational Aeroacoustics • Propulsion • Simulations • Aircraft • Research • Aircraft System Noise Assessment • Aircraft Noise Prediction • Aeroacoustic Loads • Phased Array • Cfd • Orbital Mechanics

Industries

Research

Resumes

Resumes

Yueping Guo Photo 1

Yueping Guo

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Industry:
Research
Education:
University of Cambridge 1983 - 1986
Doctorates, Doctor of Philosophy, Philosophy Tsinghua University 1977 - 1982
Bachelors, Engineering
Skills:
Fortran
Airframe Noise Modeling
Sonic Environment
Aircraft Noise Reduction
Engineering Management
Aerospace Engineering
Ray Tracing
Aeroacoustics
Fluid Mechanics
Fluid Dynamics
Numerical Analysis
Aeroelasticity
Matlab
Aerodynamics
Msc.patran
Unconventional Aircraft Acoustics
Acoustic Fatigue
Boundary Element Method
Engineering
Wind Tunnel Testing
Finite Element Analysis
Computational Aeroacoustics
Propulsion
Simulations
Aircraft
Research
Aircraft System Noise Assessment
Aircraft Noise Prediction
Aeroacoustic Loads
Phased Array
Cfd
Orbital Mechanics

Business Records

Name / Title
Company / Classification
Phones & Addresses
Yueping Guo
Principal
Abacusology Ltd Partnership
Business Services
3830 Daisy Cir, Seal Beach, CA 90740
Yueping Guo
Principal
Abacusology Limited Partnership
Business Services
3830 Daisy Cir, Seal Beach, CA 90740

Publications

Us Patents

Method And System To Account For Angle Of Attack Effects In Engine Noise Shielding Tests

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US Patent:
8532961, Sep 10, 2013
Filed:
Oct 29, 2010
Appl. No.:
12/916451
Inventors:
Yueping Guo - Seal Beach CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
H03F 1/26
B64C 1/40
G05B 13/02
G06G 7/48
US Classification:
702191, 244 1 N, 700 30, 703 8
Abstract:
There is provided a method to account for aircraft angle of attack effects in engine noise shielding in aircraft configurations having one or more engines mounted above a wing or a lifting body. The method includes computing a local flow field from a known standard full aircraft configuration oriented at a nonzero angle of attack. The method further includes computing a mean flow field in a test dataset from a small scale aircraft model test configuration oriented at a zero angle of attack. The method further includes matching the local flow field with the mean flow field to identify a selected noise measurement dataset. The method further includes rotating the selected noise measurement dataset in a far field directivity rotation angle to match the nonzero angle of attack, thus resulting in engine noise shielding results for the full aircraft configuration at the nonzero angle of attack.

Apparatus And Method For Reducing Aircraft Noise And Acoustic Fatigue

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US Patent:
20050194205, Sep 8, 2005
Filed:
Mar 4, 2004
Appl. No.:
10/792941
Inventors:
Yueping Guo - Seal Beach CA, US
International Classification:
B64F001/26
G10K011/00
E04H017/00
E04B001/82
E04B002/02
US Classification:
181210000, 181290000
Abstract:
An apparatus and method is provided for attenuating aerospace engine noise and unsteady pressure fluctuations associated with high velocity exhaust flows. The apparatus and method reduce acoustic fatigue damage to aerospace vehicles that may be caused by the reflection of exhaust energy from landing and/or launch platforms. The apparatus includes a passive treatment area associated with the platform operable for reducing the magnitude of the reflected sound waves and unsteady pressure fluctuations from the high velocity exhaust mass flow exiting from the engine. The passive treatment area may include a layer of sound absorptive material, at least one set of roughness elements for disrupting high velocity flow structures. A protective cover may be positioned over the passive treatment area for permitting exhaust flow to pass therethrough while still providing adequate structure to support the weight of the aerospace vehicle.

Low-Noise Pulse Jet Engine

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US Patent:
20070028593, Feb 8, 2007
Filed:
Aug 4, 2005
Appl. No.:
11/197692
Inventors:
Yueping Guo - Seal Beach CA, US
International Classification:
F02K 7/02
US Classification:
060204000, 060247000
Abstract:
An engine including multiple pulse ducts. Each pulse duct has a hollow interior extending from an upstream end to a downstream end for transporting high-pressure fluid. The high-pressure fluid is expelled from the downstream ends of the pulse tubes during operation of the engine. The engine further includes an ejector adjacent the downstream ends of the plurality of pulse ducts comprising a plurality of segregated compartments. Each compartment is aligned with the downstream end of a corresponding pulse duct of the plurality of pulse ducts to receive the high-pressure fluid expelled from the downstream end of the corresponding pulse duct for preventing high-pressure fluid expelled from each pulse duct from interacting with fluid expelled from each adjacent pulse duct.
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Yueping Guo from Saipan, MP Get Report