Julie Hayes

发表

Design and Development of a Deep Acoustic Lining for the 40-by 80-Foot Wind Tunnel Test Section

Marianne Mosher, Paul T. Soderman, Fredric H. Schmitz, 2002 .

AIRFRAME NOISE CHARACTERISTICS OF A 4.7% SCALE DC-10 MODEL

Julie Hayes, W. Clifton Home, Paul T. Sodermant, 1997 .

MEASUREMENT OF REYNOLDS NUMBER EFFECT ON AIRFRAME NOISE IN THE 12-FOOT PRESSURE WIND TUNNEL

Paul T. Soderman, Stephen M. Jaeger, Julie Hayes, 1999 .

Airframe noise characteristics of a 4.7 percent scale DC-10 model

Julie Hayes, Paul H. Bent, William C. Horne, 1997 .

Acoustic Quality of the 40- by 80- Foot Wind Tunnel Test Section After Installation of a Deep Acoustic Lining

Paul T. Soderman, Stephen M. Jaeger, Julie Hayes, 2002 .

Aeroacoustic study of flap-tip noise reduction using continuous moldline technology

Bruce L. Storms, Paul T. Soderman, Stephen M. Jaeger, 2000 .

Measurements of unsteady pressure fluctuations on the surface of an unswept, multi-element airfoil

Bruce L. Storms, Julie Hayes, William C. Horne, 1997 .

Acoustic performance of the 40- by 80- foot wind tunnel test section deep acoustic lining

Paul T. Soderman, Christopher S. Allen, Stephen M. Jaeger, 2000 .

Design of a deep acoustic lining for the 40- by 80-foot Wind Tunnel test section

Paul T. Soderman, Fredric H. Schmitz, Christopher S. Allen, 1999 .

Aeroacoustic measurements of slat noise on a three-dimensional high-lift system

Bruce L. Storms, Julie Hayes, James C. Ross, 1999 .

Flight Effects on the Far-Field Noise of a Heated Supersonic Jet

Paul T. Soderman, Christopher S. Allen, Stephen M. Jaeger, 1997 .

Effects of distributed source coherence on the response of phased acoustic arrays

Stephen M. Jaeger, Julie Hayes, Srba Jovic, 2000 .