Method predicts lift and pitching moment characteristics of STOL aircraft with externally-blown, jet-augmented wing-flap combinations using potential-flow approach which involves combination of two flow models. Method can accommodate multiple engines per wing panel and part-span flaps.
Calculation of aerodynamic characteristics of STOL aircraft
1974-11-01
Sonstige
Keine Angabe
Englisch
Aerodynamic Characteristics of Fan-Jet STOL Aircraft
NTIS | 1983
|Aerodynamic Problems of STOL Aircraft
NTIS | 1973
|Modeling and Approximation of STOL Aircraft Longitudinal Aerodynamic Characteristics
Online Contents | 2015
|