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- W1492650257 abstract "Summary Nonstationary statistical methods are applied in obtaining the rigid-body structural load response of a vertical-rising ballistic missile to a flight environment of atmospheric disturbances. Results are obtained for a missile of the IRBM class. The in put consists of the average and the covariance of the wind velocity at Patrick AFB during the winter months. A method which involves taking the square root of the input covariance matrix was employed in computing the covariance matrix of the response. The average and the standard deviation of the structural bend ing moment are shown at the critical flight altitude of 33,000 ft. The 99% extreme-value design loads obtained with a design criterion proposed in this paper are compared with design loads obtained with other criteria." @default.
- W1492650257 created "2016-06-24" @default.
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- W1492650257 date "1961-04-01" @default.
- W1492650257 modified "2023-09-24" @default.
- W1492650257 title "Missile Structural Loads by Nonstationary Statistical Methods" @default.
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- W1492650257 doi "https://doi.org/10.2514/8.8961" @default.
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