Nine-degree-of-freedom simulation of rotating parachute systems-Reference-Cited by-同舟云学术

Nine-degree-of-freedom simulation of rotating parachute systems

Published:1992-09 Issue:5 Volume:29 Page:774-781
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Doherr Karl-Friedrich¹,Schilling Hartmut²

Affiliation:

1. DLR-Institut fur Flugmechanik, 3300 Braunschweig, Germany

2. Rheinmetall GmbH, 4000 Dusseldorf, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46245

Reference13 articles.

1. TWolf, D. F. "The Dynamic Stability of a Non-Rigid Parachute and Payload System," Ph.D. Dissertation,Univ. of Rhode Island, Kingston, RI, 1968.

2. 3Doherr, K.F. "Theoretisch-experimentelle Untersuchung des dynamischen Verhaltens von Fallschirm-Last-Systemen bei Windkanalversuchen," Ph.D. Thesis,Technische Universitat Miinchen, DFVLR-FB81-29, Munich,1981.

3. Parachute/submunition system coupled dynamics

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