Publication Date:
2019-06-27
Description:
A simulator study of STOL airworthiness criteria was conducted using a model of an augmentor wing transport. The approach, flare and landing, go-around, and takeoff phases of flight were investigated. The results are summarized and possible implications with regard to airworthiness criteria are discussed. The results provide a data base for future STOL airworthiness requirements and a preliminary indication of potential problem areas. The results are also compared to the results from an earlier simulation of the Breguet 941S. Where possible, airworthiness criteria are proposed for consideration.
Keywords:
AERODYNAMICS
Type:
NASA-TM-X-62395
,
AD-A005878
,
FAA-RD-74-179-VOL-1
,
A-5797-VOL-1
Format:
application/pdf