Search Results - "Burley, Casey L."

Technical note: preliminary work for modeling the propellers of an aircraft as a noise source in an acoustic boundary element analysis.

Authors: Vlahopoulos, Nickolas Lyle, Karen H. Burley, Casey L.

Source: Noise Control Engineering Journal; May/June 1998, Vol. 46 Issue 3, p132-136, 5p

Hybrid wing body aircraft system noise assessment with propulsion airframe aeroacoustic experiments.

Authors: Thomas, Russell H. Burley, Casey L. Olson, Erik D.

Source: International Journal of Aeroacoustics. Sep2012, Vol. 11 Issue 3/4, p369-410. 42p.

ANOPP landing-gear noise prediction with comparison to model-scale data.

Authors: Burley, Casey L. Brooks, Thomas F. Humphreys Jr., William M. et al.

Source: International Journal of Aeroacoustics. Sep2009, Vol. 8 Issue 5, p445-475. 31p. 3 Black and White Photographs, 4 Diagrams, 3 Charts, 13 Graphs.

The HART II test – measurement of helicopter rotor wakes

Alternate Title: Der HART II Test – Messung des Nachlaufs von Hubschrauberrotoren

Authors: van der Wall, Berend G. Burley, Casey L. Yu, Yung et al.

Source: Aerospace Science & Technology. Jun2004, Vol. 8 Issue 4, p273-284. 12p.

Subjects: Fluid dynamic measurements, Rotors (Helicopters), Aerofoils, Aeronautics

Auralization of Hybrid Wing-Body Aircraft Flyover Noise from System Noise Predictions.

Authors: Rizzi, Stephen A. Aumann, Arie R. Lopes, Leonard V. et al.

Source: Journal of Aircraft; Nov/Dec2014, Vol. 51 Issue 6, p1914-1926, 13p

Jet noise shielding provided by a hybrid wing body aircraft.

Authors: Doty, Michael J. Brooks, Thomas F. Burley, Casey L. et al.

Source: International Journal of Aeroacoustics. Mar2018, Vol. 17 Issue 1/2, p135-158. 24p.

Effect of wake structure on blade-vortex interaction phenomena: Acoustic prediction and validation.

Authors: Gallman, Judith M. Schultz, Klaus-J. Spiegel, Pierre et al.

Source: Journal of Aircraft. Mar/Apr98, Vol. 35 Issue 2, p267. 7p. 1 Diagram, 2 Charts, 73 Graphs.

Subjects: Vortex motion, Mathematical models