The problems relating to path control which are encountered during landing approach with jumbo and STOL aircraft are outlined, and special consideration is given to those which occur during steep approaches used for noise abatement. The direct control of lift represents one possibility for alleviating these problems. The capabilities and limits of a DLC system such as was used in an HFB 320 Hansa are evaluated on the basis of simulation and flight test results. The preliminary empirical data from steep two-segment noise-abatement flights with the HFB 320 are reported. (Author)
Flight-Mechanics Problems During Landing Approach with Direct Lift Control, Exemplified by Hfb 320 Hansa
1974
34 pages
Report
No indication
English