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Base-Pressure Experimental Investigation on a Space Launcher in Subsonic Regime

  • Published:2013-05 Issue:3 Volume:50 Page:572-578
  • ISSN:0022-4650
  • Container-title:Journal of Spacecraft and Rockets
  • language:en
  • Short-container-title:Journal of Spacecraft and Rockets

Author:

Paciorri R.,Sabetta F.,Valenza F.,Fauci R.,Passaro A.,Baccarella D.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 6 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. Wind Tunnel Installation Effects on the Base Flow for a High-Speed Exhaust System;AIAA SCITECH 2024 Forum;2024-01-04

2. Propulsion Aerodynamics for a Novel High-Speed Exhaust System;Journal of Engineering for Gas Turbines and Power;2023-10-17

3. Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow;International Journal of Aeronautical and Space Sciences;2022-08-18

4. Numerical and Experimental Analysis of Subsonic and Transonic Base Pressure;Journal of Physics: Conference Series;2021-04-01

5. Study of Base DRAG Prediction With Chamber Pressure at Super-Sonic Flow;Journal of the Korean Society for Aeronautical & Space Sciences;2020-11-30
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