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STOVL Jet Efflux Characteristics and their Influence on Propulsion-Induced EffectsJet efflux characteristics are a determining factor in STOVL aircraft aero/propulsion induced effects. Subcritical jets may have core lengths which range up to 6 diameters. The shorter core length jets tend to entrain ambient air more rapidly, inducing larger hover lift losses, and decay more rapidly, reducing adverse ground erosion. In transition flight, shorter core length jets show a larger decrease in the lift loss and a slight decrease in nose-up pitching moment. Supercritical pressure ratio jets tend to have longer, higher pressure core lengths with a greater hazard for ground erosion. The decay in the fully developed region is similar for both subcritical and supercritical pressure ratio jets. For subsonic jets the decay is inversely proportional to the distance from the jet exit. In ground effect the supercritical jet induces an oscillating pressure distribution on the ground with reflected shocks and expansions which can increase ground erosion and, at low ground heights, cause non-monotonic lift loss variations.
Document ID
20020040849
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Arledge, Tom
(NASA Ames Research Center Moffett Field, CA United States)
Wardwell, Doug
(NASA Ames Research Center Moffett Field, CA United States)
Hange, Craig
(NASA Ames Research Center Moffett Field, CA United States)
Naumowicz, Tim
(NASA Ames Research Center Moffett Field, CA United States)
Olson, Lawrence
Date Acquired
August 20, 2013
Publication Date
January 1, 1996
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: International Powered Lift Conference
Location: West Palm Beach, FL
Country: United States
Start Date: November 18, 1996
End Date: November 21, 1996
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 505-68-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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