Investigation of the nonlinear flight dynamics of ordnance weapons-Reference-Cited by-同舟云学术

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Investigation of the nonlinear flight dynamics of ordnance weapons

Published:1970-10 Issue:10 Volume:7 Page:1241-1243
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

NICOLAIDES JOHN D.¹,INGRAM CHARLES W.¹,CLARE THOMAS A.¹

Affiliation:

1. University of Notre Dame, Noire Dame, Ind.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.30141

Reference9 articles.

1. Nicolaides, J. D., Free Flight Dynamics, Univ. of Notre Dame, Notre Dame, Ind.1961, pp.103-204.

2. FREE FLIGHT MOTION OF SYMMETRIC MISSILES

3. Ingram, C. W. "On Obtaining the Nonlinear Aerodynamic Stability Coefficients from the Free Angular Motion of a Rigid Body," Ph.D. thesis,June 1969, Univ. of Notre Dame, Notre Dame, Ind.

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