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A Parametric Approach to Hover Balance Analysis of Two STOVL Fighter Concepts NASA Ames Research Center, Moffett Field, CA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Samuels, Jeffrey J., author.
Conference Name:
SAE Aerospace Technology Conference and Exposition (1986-10-13 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1986
Summary:
Successful 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
Notes:
Vendor supplied data
Publisher Number:
861631
Access Restriction:
Restricted for use by site license

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