Paul T. Soderman

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 .

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

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

Sources and levels of background noise in the NASA Ames 40- by 80-foot wind tunnel

Paul T. Soderman, 1988 .

Array Design and Performance for a Large Scale Airframe Noise Study

Nathan Burnside, Paul T. Soderman, Stephen M. Jaeger, 2002 .

Microphone Corrections for Accurate In-Flow Acoustic Measurements at High Frequency

Paul T. Soderman, Christopher S. Allen, Kartik Vandra, 1994 .

Summary of HEAT 1 Aeroacoustics Installation Effects

Paul T. Soderman, Brian E. Smith, Fanny A. Zuniga, 1999 .

Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80 Foot Wind Tunnel

Nathan Burnside, Paul T. Soderman, William C. Horne, 2005 .

Improving Large-Scale Testing Capability by Modifying the 40- by 80-ft Wind Tunnel

Paul T. Soderman, Kenneth W. Mort, William T. Eckert, 1979 .

Airframe Noise Study of a CRJ-700 Aircraft Model in the NASA Ames 7- by 10- Foot Wind Tunnnel No. 1

Nathan Burnside, Paul T. Soderman, Stephen M. Jaeger, 2002 .

The Prediction of STOVL Noise- Current Semi-Empirical Methods and Comparisons with Jet Noise Data

Paul T. Soderman, 1990 .

Measurement of Model Noise in a Hard-Wall Wind Tunnel

Paul T. Soderman, 2006 .

Acoustic and aerodynamic study of a pusher-propeller aircraft model

Paul T. Soderman, W. Clifton Horne, W. Horne, 1990 .

MICROPHONE ARRAY ASSESSMENT OF AN ISOLATED, 26%-SCALE, HIGH-FIDELITY LANDING GEAR

Nathan Burnside, Paul T. Soderman, Stephen M. Jaeger, 2002 .

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 .

Investigation of Acoustic Effects of Leading-Edge Serrations on Airfoils

Paul T. Soderman, Richard E. Hayden, Alan S. Hersh, 1974 .

Aeroacoustic Study of a 26%-Scale Semispan Model of a Boeing 777 Wing in the NASA Ames 40- by 80-Foot Wind Tunnel

Nathan Burnside, Paul T. Soderman, Stephen M. Jaeger, 2004 .

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

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

Aeroacoustic Research Techniques: Jets to Autos

Paul T. Soderman, 1999 .

Current Background Noise Sources and Levels in the NASA Ames 40- by 80-Foot Wind Tunnel: A Status Report

Dennis Koga, Paul T. Soderman, Stephen M. Jaeger, 1999 .

The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

Paul T. Soderman, Larry E. Olson, L. Olson, 1992 .

Aerodynamic Flow Quality and Acoustic Characteristics of the 40- by 80-Foot Test Section Circuit of the National Full-Scale Aerodynamic Complex

Paul T. Soderman, Lawrence E. Olson, Peter T. Zell, 1987 .

Acoustic Modifications of the Ames 40x80 Foot Wind Tunnel and Test Techniques for High-Speed Research Model Testing

Paul T. Soderman, Larry E. Olson, 1995 .

Ames Hybrid Combustion Facility

Daniel P. Bencze, Paul T. Soderman, Greg Zilliac, 2003 .

J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field

Paul T. Soderman, Adolph Atencio, Alain Julienne, 1991 .

Internal Acoustics Measurements of a Full Scale Advanced Ducted Propulsor Demonstrator

Paul T. Soderman, M. G. Jones, O. L. Santa Maria, 1995 .

Measurements of Forward Flight Effects on the Advanced Ducted Propulsion Demonstrator Engine

Paul T. Soderman, Lawrence Olson, W. C. Horne, 1994 .

A directional microphone array for acoustic studies of wind tunnel models

Paul T. Soderman, Stephen C. Noble, 1975 .

Aeroacoustics analysis and community noise overview

Robert A. Golub, Paul T. Soderman, 1992 .

Microphone Measurements In and Out of Airstream

Paul T. Soderman, Christopher S. Allen, 2002 .

Reduction of Background Noise in the NASA Ames 40- by 80-Foot Wind Tunnel

Paul T. Soderman, Stephen M. Jaeger, Christopher S. Allen, 1995 .

Oblique incidence sound absorption of porous materials covered by perforated metal and exposed to tangential airflow

Paul T. Soderman, 1982 .

Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel

Paul T. Soderman, Larry E. Olsen, 1990 .

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 .

Aerodynamic design of gas and aerosol samplers for aircraft

Paul T. Soderman, William H. Brune, W. Brune, 1991 .

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 .

Noise of the Harrier in vertical landing and takeoff

Paul T. Soderman, John D. Foster, 1988 .

Improving large-scale testing capability by modifying the 40- by 80-foot wind tunnel

Paul T. Soderman, Kenneth W. Mort, William T. Eckert, 1977 .

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

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

Airframe Noise Study of a Bombardier CRJ-700 Aircraft Model in the NASA Ames 7-by 10-Foot Wind Tunnel

Nathan Burnside, Paul T. Soderman, Stephen M. Jaeger, 2004 .

On the scaling of small-scale jet noise to large scale

Paul T. Soderman, Christopher S. Allen, 1992 .

Aeroacoustic probe design for microphone to reduce flow-induced self-noise

Paul T. Soderman, Cristopher S. Allew, 1993 .

Flow-field Survey of an Empennage Wake Interacting with a Pusher Propeller

Paul T. Soderman, W. Clifton Horne, 1988 .