The Investigation of Take-off and Landing Characteristics of Jet Shortened Take-off and Landing Aircraft (STOL) (K Voprosu Issledovaniya Vzletno-Posadochnykh Kharakteristik Reaktivnykh Samoletov Ukorochennogo Vzleta i Posadki (SUVP)).

摘要

The negative effect of secondary forces induced by the jet flow of the engine because of its ejection properties is not taken into account during the examination of aerodynamic and take-off and landing characteristics of jet STOL and VTOL aircraft (vertical take-off and landing aircraft). It can be so significant for certain STOL configurations (Figure 1) that aircraft equipped with a BLC system (boundary layer control) could be more preferable.