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Structural-Acoustic Simulations in Early Airframe Design

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
83892
Program Year/Program:
2007 / SBIR
Agency Tracking Number:
065931
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
MICHIGAN ENGINEERING SERVICES, LLC
2890 Carpenter Road, Suite 1900 Ann Arbor, MI -
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2007
Title: Structural-Acoustic Simulations in Early Airframe Design
Agency: NASA
Contract: NNL07AA78P
Award Amount: $99,993.00
 

Abstract:

The structural design during the early development of an aircraft focuses on strength, fatigue, corrosion, maintenance, inspection, and manufacturing. Usually the acoustic requirements are met after the design of the fuselage structure has been completed. Ideally the structural-acoustic concerns should enter the design cycle early and they should be considered along with other main design disciplines within a Multi-disciplinary Design Optimization (MDO) environment. The proposing firm is uniquely positioned for developing technology which will bring structural-acoustic simulations early in the airframe design process because of their Energy Finite Element Analysis (EFEA) product for structural-acoustic simulations of large systems, and their development of a general purpose code for Multi-disciplinary Design Optimization under Uncertainty (MDO-U). The proposed Phase I project will demonstrate the feasibility of including structural-acoustic simulations in early airframe design. An adjoint sensitivity formulation will be implemented in the EFEA for enabling the utilization of the EFEA within a design optimization environment. In a case study a representative airframe structure will be optimized simultaneously for two different disciplines, using common design variables. An impact type of concern (representative of impact applications for rotorcraft and aircraft, and of shock applications for launch vehicle dynamics) and a structural-acoustic performance due to structure-borne and air-borne excitations (representative to aircraft, rotorcraft, and launch vehicle applications) will be considered. The MDO-U and the EFEA codes will be utilized in the case study, which will demonstrate the feasibility and the value of bringing structural-acoustics early in the design cycle.

Principal Investigator:

Geng O. Zhang
Principal Investigator
7344775710
gengzhang@miengsrv.com

Business Contact:

Christina P. Vlahopoulos
Business Official
7343580777
christinavl@miengsrv.com
Small Business Information at Submission:

Michigan Engineering Services, LLC
2890 Carpenter Road, Suite 1900 Ann Arbor, MI 48108

EIN/Tax ID: 900100742
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No