Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation
Latest Publications

TOTAL DOCUMENTS

35

(FIVE YEARS 0)

H-INDEX

1

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9780915928026, 9781600865121

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Highly Noise-Suppressed Bypass 6 Engine for STOL Application

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0141.0156 ◽

1975 ◽

pp. 141-156

Download Full-text

Sound Generation by Wake Cutting

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0035.0041 ◽

1975 ◽

pp. 35-41

Keyword(s):

Sound Generation

Download Full-text

Comparison of Results Obtained with Various Sensors Used to Measure Fluctuating Quantities in Jets

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0451.0466 ◽

1975 ◽

pp. 451-466

Keyword(s):

Comparison Of Results

Download Full-text

Inlet Geometry and Axial Mach Number Effects on Fan Noise Propagation

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0073.0094 ◽

1975 ◽

pp. 73-94

Keyword(s):

Mach Number ◽

Fan Noise ◽

Noise Propagation ◽

Inlet Geometry

Download Full-text

Response of Panels to Turbulence-Induced, Surface-Pressure Fluctuations and Resulting Acoustic Radiation to the Flowfield

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0203.0224 ◽

1975 ◽

pp. 203-224

Keyword(s):

Surface Pressure ◽

Acoustic Radiation ◽

Pressure Fluctuations

Download Full-text

Sonic Boom Analysis for High-Altitude Flight at High Mach Number

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0301.0320 ◽

1975 ◽

pp. 301-320

Keyword(s):

Mach Number ◽

High Altitude ◽

Sonic Boom ◽

High Mach Number ◽

High Mach

Download Full-text

Unsteady Aerodynamic Loads on Slender Cones at Freestream Mach Numbers from 0 to 22

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0285.0296 ◽

1975 ◽

pp. 285-296

Keyword(s):

Aerodynamic Loads ◽

Unsteady Aerodynamic ◽

Mach Numbers

Download Full-text

Mechanisms of Externally Blown Flap Noise

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0113.0128 ◽

1975 ◽

pp. 113-128

Download Full-text

Pressure Fluctuations Underlying Attached and Separated Supersonic Turbulent Boundary Layers and Shock Waves

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0243.0262 ◽

1975 ◽

pp. 243-262

Keyword(s):

Shock Waves ◽

Boundary Layers ◽

Pressure Fluctuations ◽

Turbulent Boundary Layers ◽

And Shock Waves

Download Full-text

Flap Noise Prediction Method for a Powered Lift System

Aeroacoustics: Fan, STOL, and Boundary Layer Noise; Sonic Boom; Aeroacoustics Instrumentation ◽

10.2514/5.9781600865121.0099.0112 ◽

1975 ◽

pp. 99-112

Keyword(s):

Prediction Method ◽

Noise Prediction

Download Full-text