Aerothermal Enviroment Definition for A Reusable Experimental Re-Entry Vehicle Wing-Reference-Cited by-同舟云学术

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Aerothermal Enviroment Definition for A Reusable Experimental Re-Entry Vehicle Wing

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Thermophysics Conference
language:
Short-container-title:

Author:

Battista Francesco¹,Rufolo Giuseppe¹,Di Clemente Marco¹

Affiliation:

1. CIRA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4048

Reference20 articles.

1. SolazzoM.etal,"USV-XConceptualDesign,Analysis and Calculation Data Package",CIRA-CF-05-0957.

2. Di Clemente M., Battista F., Rufolo G.C. "Time history of heat flux and pressure over the FTB_X wing along the ORT trajectory", CIRA CF-06-0154.

3. Salvatore,Solazzo,Filippone,Schettino,Battista,Pezzella,Votta, `USV-XPhaseA activityreport',CIRA-CF-06-823.

4. Schettino,E.Bucchignani,"SoftwareandNumerical Design of H3NS",CIRA-TR-AEP-99-126.

5. ParkC."AReview of Reaction Ratesin HighTemperatureAir", AIAA paper89-1740,June1989.

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1. Landing Gear Concept and Dynamic Landing Loads of the Unmanned Space Re-entry Vehicle USV3;Procedia Engineering;2015

2. Gradient-based Aerothermodynamic Optimization of a Hypersonic Wing Profile;Procedia Engineering;2015

3. The Conceptual Structural Design of an Unmanned Space Vehicle with Re-entry and Landing Capabilities;14th AIAA Aviation Technology, Integration, and Operations Conference;2014-06-13

4. Aerodynamic database development of the ESA intermediate experimental vehicle;Acta Astronautica;2014-01

5. Hypersonic environment assessment of the CIRA FTB-X re-entry vehicle;Aerospace Science and Technology;2013-03

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