Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel-Reference-Cited by-同舟云学术

Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Pinier Jeremy¹,Niskey Charles¹,Hanke Jeremy¹,Tomek William¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-998

Reference8 articles.

1. 2Hanke, J.L."TestSummaryfor1MomentModelTestingintheBoeingPolysonic WindTunnel,PSWTTest850,"Ares-AD-TA-0010,2008.

2. 3Pinier, J. T. "0.01-Scale Ares I Crew Launch Vehicle ADAC-3 (A106) Force and Moment testing at the Boeing Polysonic Wind Tunnel," Ares-AD-TA-0024,2010.

3. 4Erickson, G. E. "0.01-Scale CLV DAC-2A Force and Moment Model Testing in the NASA Langley Research Center Unitary Plan Wind Tunnel, UPWTTests 1968/1813," Ares-AD-TA-0004,2007.

Cited by 10 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. Detailed Uncertainty Analysis of the Ares I A106 Liftoff/Transition Database;Journal of Spacecraft and Rockets;2012-09

2. Assessment of Computational-Fluid-Dynamics-Based Response Surface Database for Ares I Supersonic Ascent Aerodynamics;Journal of Spacecraft and Rockets;2012-07

3. Error Estimates of the Ares I Computed Turbulent Ascent Longitudinal Aerodynamic Analysis;Journal of Spacecraft and Rockets;2012-07

4. Liftoff and Transition Aerodynamics of the Ares I Launch Vehicle;Journal of Spacecraft and Rockets;2012-07

5. Detailed Uncertainty Analysis of the Ares I A106 Liftoff/Transition Database;29th AIAA Applied Aerodynamics Conference;2011-06-27