5 Figure 2. Wing and Landing Gear Contributions to Total Airframe Noise for Baseline Business Jet and Boeing 737 at Approach. 6 Figure 3. ... Schematic Diagram of the Slat/Wing Model and Elevation Angle Position (Side View). 22 Figure 14.
Title | : | Small Engine Technology (SET). Task 33: Airframe, Integration, and Community Noise Study |
Author | : | |
Publisher | : | - 2002 |
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