NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Analytical study of STOL Aircraft in ground effect. Part 2: Nonplanar, nonlinear method applicable to three dimensional jets of finite thicknessThe ability of the potential flow analysis (POTFAN) to predict the influence of ground proximity on lift systems is examined. A two dimensional study employing vortex lattice methodology provides confidence that ground effect phenomenon can be predicted using discrete singularity representation. Two dimensional quasi-steady ascent and descent behavior determined provides guidance in interpreting three dimensional results. Steady and quasi-steady ground effect aerodynamic characteristics predicted by POTFAN are presented for several basic unpowered configurations. POTFAN results are compared with experimental data and results of other analytical methods. Modification of POTFAN to incorporate multienergy flow analysis is discussed. General aspects of thick jet models are examined to provide a basic for extending POTFAN's scope to include analysis of propulsive lift interactions.
Document ID
19810010571
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shollenberger, C. A.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-152088-PT-2
Report Number: NASA-CR-152088-PT-2
Accession Number
81N19097
Funding Number(s)
CONTRACT_GRANT: NAS2-9319
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available