Accurate gust load calcuations for three short haul aircraft were used to compare: (1) PSD are discrete gust methods, (2) PSD mission analysis and design envelope results, and (3) PSD results for vertical and lateral gusts. These data are also used to study in detail problems of T-tails. (Author)
Rational Calculation of Design Gust Loads in Relation to Present and Proposed Airworthiness Requirements
1972
13 pages
Report
Keine Angabe
Englisch
New aircraft-engine airworthiness requirements are proposed
Engineering Index Backfile | 1932
Evolution of airplane gust loads design requirements
AIAA | 1995
|Evolution of Airplane Gust Loads Design Requirements
Online Contents | 1995
|U.S. Airworthiness Requirements
Emerald Group Publishing | 1933