To establish launch vehicle loads during atmospheric flight, the statistical characteristics of the turbulence/gust-induced loads need to be determined. Recently, a Monte Carlo analysis procedure was developed that uses measured turbulence/gusts to establish launch vehicle loads. This paper presents the procedures developed to characterize the distribution of the data and to calculate tolerance bounds on these Monte Carlo loads.
Statistical Analysis of Atmospheric Flight Gust Loads Analysis Data
1999
28 pages
Report
Keine Angabe
Englisch
Statistical Analysis of Atmospheric Flight Gust Loads Analysis Data
British Library Conference Proceedings | 1999
|Atmospheric Flight Gust Loads Analysis
British Library Conference Proceedings | 1999
|