Aerodynamic Measurements in a Wind Tunnel on Scale Models of a 777 Main Landing Gear
Aerodynamic measurements were taken over models of the Boeing 777 high fidelity isolated landing gear in the 6- by 6-foot Virginia Tech Stability Wind Tunnel (VT-SWT) at a free-stream Mach number of 0.16. Noise control devices (NCD) were developed at Virginia Tech [9] to reduce noise by shielding ge...
Main Author: | Ringshia, Aditya K. |
---|---|
Other Authors: | Mechanical Engineering |
Format: | Others |
Published: |
Virginia Tech
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/34583 http://scholar.lib.vt.edu/theses/available/etd-08162006-155652/ |
Similar Items
-
Wind Tunnel Tests for a Pitot-Static Probe Designed to Measure Aircraft Speed and Altitude at Subsonic Compressible and Transonic Regimes
by: Hasan TABANLI, et al.
Published: (2021-07-01) -
Analysis of Applicability of Flow Averaging Pitot Tubes in the Areas of Flow Disturbance
by: Pochwała Sławomir, et al.
Published: (2016-03-01) -
Computational Evaluation of Aerodynamic Loading on Retractable Landing-Gears
by: Giuliano De Stefano, et al.
Published: (2020-05-01) -
Composite skid landing gear design investigation
by: Shrotri, Kshitij
Published: (2008) -
Supersonic and transonic Mach probe for calibration control in the Trisonic Wind Tunnel
by: Alexandru Marius PANAIT
Published: (2017-12-01)