Experimental study of the effect of blade curvature and aspect ratio on the performance of a rotary-wing decelerator-Reference-Cited by-同舟云学术

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Experimental study of the effect of blade curvature and aspect ratio on the performance of a rotary-wing decelerator

Published:2015-06 Issue: Volume:43 Page:471-477
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Martiarena Juan Francisco,Nadal Mora Vicente,Piechocki Joaquín

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Concept options for the aerial survey on Titan;Dorrington;Adv. Space Res.,2011

2. The guided samara: design and development of a controllable single-bladed autorotating vehicle;Kellas,2007

3. T.J. Steiner, L.A. Young, Rotary wing decelerator use on Titan, in: Internationally Planetary Probe Workshop 8, EEUU, Portsmouth, 2011.

4. Rotary-wing decelerators for probe descent through the atmosphere of Venus;Young,2004

5. Analysis of samara-wing decelerator steady-state characteristics;Crimi;J. Aircr.,1988

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