The flight characteristics and boundary conditions which affect a steep approach are described for rotary wing aircraft. The limits for steep instrument approach are presented, and experiences in flight operation are depicted. Essential advantages are shown for a flight path angle of 15 deg over the ILS approach. Some necessary prerequisites for a steep landing approach by instruments are briefly considered.
Steep Approach Limits for Rotary Wing Aircraft ueber die Grenzen von Steilanfluegen MIT Drehflueglern
1973
8 pages
Report
Keine Angabe
Englisch
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