Propulsion System Impact on Military/Commercial STOL Transport Commonality

Format:

Conference/Event

Author/Creator:

Stalder, J. P., author.

Conference Name:

National Air Transportation Meeting (1970-04-20 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1970

Summary:

A STOL medium tactical transport featuring 1000 ft takeoff distance performance has been established utilizing the powered-lift wing to achieve STOL capability. Two powered-lift wing concepts, the augmented jet flap and the externally blown flap, are presented as optimum for a minimum thrust-to-weight ratio configuration. Interconnecting the propulsion system with engine cross ducting minimizes the unsymmetrical lift resulting from an engine failure. A commercial counterpart to the military transport is discussed

Notes:

Vendor supplied data

Publisher Number:

700269

Access Restriction:

Restricted for use by site license