NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
STOL aircraft flight and landing area considerations.One proposed solution to the total short-haul transportation system problem is to use existing low-wing-loading turbopropeller STOL aircraft. Deflected slipstream turboprop aircraft have also been considered for early STOL service. Aspects of current aircraft research are discussed together with the NASA research aircraft, field length and aircraft performance considerations, crosswind landings, crosswind reducing fences, elevated STOL ports, a guaranteed friction STOL runway, and problems of runway containment.
Document ID
19730046587
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Riebe, J. M.
(NASA Langley Research Center Low-Speed Aircraft Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1973
Subject Category
Facilities, Research, And Support
Report/Patent Number
ASCE PREPRINT 1726
Report Number: ASCE PREPRINT 1726
Accession Number
73A31389
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available