The Effect of Propulsion System Parameters on Vertical Take-Off and Landing Performance of a Transport Aircraft

Format:

Conference/Event

Author/Creator:

Zabinsky, Joseph M., author.

Conference Name:

SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1964

Summary:

The ability of V/STOL aircraft to take off and land vertically, while at the same time maintaining balance and control in the event of engine failure, requires selection of a propulsion system that satisfies all requirements of trim, control, and engine-out. This paper discusses the variables of those system parameters that affect aircraft take-off and landing, and also provides data to aid in evaluating the compromise necessary for selecting an adequate and efficient propulsion system

Notes:

Vendor supplied data

Publisher Number:

640235

Access Restriction:

Restricted for use by site license