INVESTIGATION ON SOUND FIELD MODEL OF PROPELLER AIRCRAFT—THE EFFECT OF RIGID FUSELAGE BOUNDARY

✍ Scribed by T.Q. Wang; S. Zhou

• Publisher: Elsevier Science
• Year: 1998
• Tongue: English
• Weight: 248 KB
• Volume: 209
• Category: Article
• ISSN: 0022-460X
• DOI: 10.1006/jsvi.1997.1231