Experimental studies of a Ludwieg tube high Reynolds number transonic tunnel-Reference-Cited by-同舟云学术

Experimental studies of a Ludwieg tube high Reynolds number transonic tunnel

Published:1973-01-10 Issue: Volume: Page:
ISSN:
Container-title:11th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

STARR R.¹,SCHUELER C.¹

Affiliation:

1. ARO, Inc., von Karman Gas Dynamics Facility, Arnold Air Force Station, Tenn.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1973-212

Reference34 articles.

1. Determination of Optimum Operating Parameters for the AEDC-PWT 4-Ft Transonic Tunnel with Variable Porosity Test Section Walls

2. Calibration of the AEDC-PWT 4-Ft. Transonic Tunnel with Modified Walls

3. 'Boone, J. R. and McCanless, G. F. "Applica- lion of the Technique for Evaluating the Acoustic Sources of Background Noise in Wind Tunnel Facilities," Tech. Report HSM-ROS-69, NASA CR 102623, Chrysler Corp., Huntsville, Ala., March 19G9.

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Study of a Transonic Wingtip Flow;30th International Symposium on Shock Waves 2;2017

2. Interference Drag Modeling and Experiments for a High-Reynolds-Number Transonic Wing;Journal of Aircraft;2012-11

3. Interference Drag Modeling and Experiments for a High Reynolds Number Transonic Wing;29th AIAA Applied Aerodynamics Conference;2011-06-27

4. Refurbishment and Testing Techniques in a Transonic Ludwieg Tunnel;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

5. Force Measurement in a Ludwieg Tube Tunnel;Journal of Spacecraft and Rockets;2007-01