The research accomplishments of the Structural Dynamics Division for F.Y. 1991 are presented. The work is discussed in terms of highlights of accomplishments during the past year and plans for the current year as they relate to 5-year plans and the objectives of each technical area. Included is research on unsteady aerodynamics, helicopter rotors, computational fluid dynamics, oscillations of leading edge flaps of a delta wing, and aircraft wing loads.
Structural Dynamics Division Research and Technology Accomplishments for Fiscal Year 1990 and Plans for Fiscal Year 1991
1991
225 pages
Report
Keine Angabe
Englisch