Parafoil aerodynamic characteristics derived from flight measured suspension system loads
Author:
Affiliation:
1. NASA, Johnson Space Center, Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1734
Reference4 articles.
1. ' Machin, R., Stein, J. and Muratore, J. "An Overview of the X-38 Prototype Crew Return Vehicle Developmentand Test Program," AIAA Paper 99-1703, to be presented at the 15* CEAS/AIAA Aerodynamic Decelerator Systems Conference& Seminar,Toulouse,France,June1999.
2. ' Iacomini, C. and Cerirnele, C. "Longitudinal Aerodynamics from a Large Scale Parafoil Test Program,"AIAA Paper99-1732,to be presentedat the 15' CEASIAIAA Aerodynamic Decelerator SystemsConference& Seminar,Toulouse,France, June1999.
Cited by 3 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. Simulation of the Baseline Performance Characteristics of a Ram-Air Parachute;24th AIAA Aerodynamic Decelerator Systems Technology Conference;2017-06-02
2. Updated flight performance and aerodynamics from a large scale parafoil test program;Modeling and Simulation Technologies Conference;2000-08-14
3. Longitudinal aerodynamics from a large scale parafoil test program;15th Aerodynamic Decelerator Systems Technology Conference;1999-06-08
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