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