Challenges and Opportunities for Noise Reduction Through Advanced Aircraft Propulsion Airframe Integration and Configurations

Aircraft noise has been a public concern since the beginning of commercial jet powered aviation. Historical progress in noise reduction has been significant and largely made possible through land use planning, noise certification, and investment into low noise technology development. More recent progress however shows increasingly diminishing returns and suggests that new avenues may need to be discovered to pursue the aggressive noise reduction goals of the present and the future. This paper focuses on the research efforts of NASA in Propulsion Airframe Aeroacoustics (PAA) through advanced engine installations and configurations, which is offered as an avenue that has potential to provide significant noise reduction. PAA is further defined and the classification tree is presented as a means of organizing PAA effects. Several aircraft configurations and engine installations, both conventional and advanced, that are designed to take advantage of airframe shielding of engine noise are presented and discussed from both a PAA and a general design perspective. Other, non-shielding related PAA opportunities are also presented. Challenges to the eventual introduction of advanced aircraft configurations are discussed.

[1]  A. S. Halm,et al.  Comparison of Low and High Nacelle Subsonic Transport Configurations , 1997 .

[2]  Brian G. Allan,et al.  Numerical Modeling of Active Flow Control in a Boundary Layer Ingesting Offset Inlet , 2004 .

[3]  Russell M. Cummings,et al.  Rethinking the Airplane Design Process - An Early 21st Century Perspective , 2004 .

[4]  Jeffrey J. Berton Noise Reduction Potential of Large, Over-the-Wing Mounted, Advanced Turbofan Engines , 2000 .

[5]  Craig Hange Trajectory Kinematics of a Simultaneous Non-Interfering Landing Approach, and the Impact on ESTOL Regional Transport Performance and Flight Control , 2003 .

[6]  Andy Ko,et al.  Assessment of the Potential Advantages of Distributed-Propulsion for Aircraft , 2003 .

[7]  L. R. Clark,et al.  Inlet Noise Reduction by Shielding for the Blended-Wing-Body Airplane , 1999 .

[8]  John-Paul Clarke,et al.  Community Noise Reduction Using Continuous Descent Approach: A Demonstration Flight Test at Louisville , 2003 .

[9]  Krishan K. Ahuja,et al.  Noise Reduction Through Circulation Control , 2001 .

[10]  P. Skully Recent Advances in Aircraft Noise Reduction , 1973 .

[11]  Marilyn J. Smith,et al.  Development of circulation control technology for application to advanced subsonic transport aircraft , 1993 .

[12]  Karl A. Geiselhart,et al.  Integration of Propulsion-Airframe-Aeroacoustic Technologies and Design Concepts for a Quiet Blended-Wing-Body Transport , 2004 .

[13]  Russell M. Cummings,et al.  From farther, faster, higher to leaner, meaner, greener: Further directions in aeronautics , 2004 .