Optimum relaxation time for a Maxwell core during forced vibration of a rocket assembly-Reference-Cited by-同舟云学术

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Optimum relaxation time for a Maxwell core during forced vibration of a rocket assembly

Published:1970-12 Issue:12 Volume:8 Page:2300-2302
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

SHAFFER BERNARD W.¹,SANN ROBERT I.²

Affiliation:

1. New York University, New York, N. Y.

2. Ingersoll Rand Research Center, Princeton, N. J.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.6116

Reference5 articles.

1. Use of Rouse's stability parameter in determining the critical layerheight of a laminar boundary layer

2. Unusual boundary-layer transition results on cones in hypersonic flow.

3. Forced Transverse Vibration of a Solid Viscoelastic Cylinder Bonded to a Thin Casing

4. Free Transverse Elastic Vibration of a Solid Cylinder Bonded to a Thin Casing

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