Expanding the Wall Interference Effect Correction Capability in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel for Semi-Span and Automotive Applications-Reference-Cited by-同舟云学术

Expanding the Wall Interference Effect Correction Capability in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel for Semi-Span and Automotive Applications

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
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Author:

Goulding Patrick W.¹,Nykamp Christopher M.¹,Czlapinski Craig²

Affiliation:

1. National Full-Scale Aerodynamics Complex

2. Navistar, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2115

Reference9 articles.

1. Developing a Robust Wall Interference Correction Methodology for Fixed-Wing Testing at the National Full-Scale Aerodynamics Complex

2. Verification of the Hensel Blockage Correction in the National Full-Scale Aerodynamics Complex 40- by 80-foot Wind Tunnel Using Hypersonic Inflatable Aerodynamic Decelerators

3. Verification and Expansion of the Hensel Blockage Correction in the National Full-Scale Aerodynamics Complex 80- by 120-foot Wind Tunnel

4. Developing a Semi-Span Wall Interference Correction Capability in the National Full-Scale Aerodynamics Complex 40- by 80-foot Wind Tunnel

5. Developing a Wall Interference Effects Correction Technique for High-Lift and Rotor Configurations in the National Full-Scale Aerodynamics Complex

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