70 results on '"Bahr, Christopher J."'
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2. Velocity discontinuity propagation model validation using an approximate point source in motion
3. Wavenumber–frequency deconvolution of aeroacoustic microphone phased array data of arbitrary coherence
4. Automated classification of transient contamination in stationary acoustic data
5. A plasma-based non-intrusive point source for acoustic beamforming applications
6. Automated Classification of Transient Contamination in Stationary Acoustic Data
7. Experimental Study of Noise Shielding by a NACA 0012 Airfoil
8. Accounting for the Influence of Decorrelation in Microphone Phased Array Deconvolution Methods
9. Phased Array Characterization of Slat Noise Radiation from a High-Lift Common Research Model
10. Unsteady Propagation and Mean Corrections in Open-Jet and Kevlar® Wind Tunnels
11. Computational Design of a Krueger Flap Targeting Conventional Slat Aerodynamics
12. A Comparison of the Noise Characteristics of a Conventional Slat and Krueger Flap
13. NASA Hybrid Wing Aircraft Aeroacoustic Test Documentation Report
14. Toward Relating Open- and Closed-Test Section Microphone Phased Array Aeroacoustic Measurements
15. Overview of Aeroacoustic Testing of the High-Lift Common Research Model
16. Characterization of Flap Edge Noise Radiation from a High-Fidelity Airframe Model
17. Advanced Background Subtraction Applied to Aeroacoustic Wind Tunnel Testing
18. Effects of resistive windscreens and foam inserts on the acoustic response of an in-flow phased microphone array
19. Shielding of Turbomachinery Broadband Noise from a Hybrid Wing Body Aircraft Configuration
20. Acoustic Data Processing and Transient Signal Analysis for the Hybrid Wing Body 14- by 22-Foot Subsonic Wind Tunnel Test
21. Jet Noise Shielding Provided by a Hybrid Wing Body Aircraft
22. Development of a Microphone Phased Array Capability for the Langley 14- by 22-Foot Subsonic Tunnel
23. System Noise Assessment and the Potential for a Low Noise Hybrid Wing Body Aircraft with Open Rotor Propulsion
24. Open Rotor Tone Shielding Methods for System Noise Assessments Using Multiple Databases
25. Hybrid Wing Body Aircraft Acoustic Test Preparations and Facility Upgrades
26. Characterization of Hybrid Wind Tunnel Environments Using Laser-Induced Acoustic Sources
27. Wavespace-Based Coherent Deconvolution
28. A review of acoustic imaging methods using phased microphone arrays
29. Fifth Workshop on Benchmark Problems for Airframe Noise Computations (BANC-V); Category 1: Trailing-Edge Noise
30. Assessment of Unsteady Propagation Characteristics and Corrections in Aeroacoustic Wind Tunnels Using an Acoustic Pulse
31. Experimental Study of Noise Shielding by a NACA 0012 Airfoil
32. Jet noise shielding provided by a hybrid wing body aircraft
33. Simulations & Measurements of Airframe Noise: A BANC Workshops Perspective
34. Subspace-based background subtraction applied to aeroacoustic wind tunnel testing
35. Editorial
36. A Microphone Array Method Benchmarking Exercise using Synthesized Input Data
37. A Comparison of Microphone Phased Array Methods Applied to the Study of Airframe Noise in Wind Tunnel Testing
38. Third Workshop on Benchmark Problems for Airframe Noise Computations (BANC-III); Category 1: Trailing-Edge Noise
39. Computational Design of a Krueger Flap Targeting Conventional Slat Aerodynamics
40. A Comparison of the Noise Characteristics of a Conventional Slat and Krueger Flap
41. Problem Statement for the AIAA/CEAS Second Workshop on Benchmark Problems for Airframe Noise Computations (BANC-II)
42. Characterization of Flap Edge Noise Radiation from a High-Fidelity Airframe Model
43. Advanced Background Subtraction Applied to Aeroacoustic Wind Tunnel Testing
44. Jet Noise Shielding Provided by a Hybrid Wing Body Aircraft
45. Calibrations of the NASA Langley 14- by 22-Foot Subsonic Tunnel in Acoustic Configuration
46. Shielding of Turbomachinery Broadband Noise from a Hybrid wing Body Aircraft Configuration
47. Acoustic Data Processing and Transient Signal Analysis for the Hybrid Wing Body 14- by 22-Foot Subsonic Wind Tunnel Test
48. Development of a Microphone Phased Array Capability for the Langley 14- by 22-foot Subsonic Tunnel
49. Open Rotor Tone Shielding Methods for System Noise Assessments Using Multiple Databases
50. System Noise Assessment and the Potential for Low Noise Hybrid Wing Body Aircraft with Open Rotor Propulsion
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