Fluid Mass Associated with an Axisymmetric Parachute Canopy-Reference-Cited by-同舟云学术

Fluid Mass Associated with an Axisymmetric Parachute Canopy

Published:1977-06 Issue:6 Volume:14 Page:577-580
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Klimas Paul C.¹

Affiliation:

1. Sandia Laboratories, Albuquerque, N. M.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.58823

Reference6 articles.

1. Elliptic integral representation of axially symmetric flows

2. 3Trulin, D. V. "A Method for Computing the Pressure Distribution about an Axisymmetric Nacelle in Subsonic Flow," Ph.D. Thesis,Iowa State University, Ames, Iowa, 1968.

3. 4Ibrahim, S. K. "Apparent Added Mass and Moment of Inertia of Cup-Shaped Bodies in Unsteady Incompressible Flow," Ph.D Thesis,University of Minnesota, May 1965.

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