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A parametric approach to hover balance analysis of two STOVL fighter conceptsSuccessful development of an aircraft with vertical landing capability must address the critical problem of balancing the aircraft for hover. In this paper a parametric method for balancing short takeoff and vertical landing (STOVL) aircraft in hover is described and applied to the analysis of two conceptual STOVL fighters. One uses a remote augmented lift system and the other a thrust-vectoring hybrid tandem-fan engine.
Document ID
19870042362
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Samuels, Jeffrey J. (NASA Ames Research Center Moffett Field, CA, United States)
Hahn, Andrew S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 861631
Accession Number
87A29636
Distribution Limits
Public
Copyright
Other

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