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Lockheed Advanced Lift Fuel Conservative Short-Haul Airliner Concepts
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<blockquote data-quote="Triton" data-source="post: 77663" data-attributes="member: 3324"><p>Renshaw, J. H.; <em>et al</em>. <em>Evaluation of Advanced Lift Concepts and Fuel Conservative Short-Haul Aircraft, Volume 1 </em> Lockheed Aircraft Corporation June 1974</p><p></p><blockquote><p>The performance and economics of a twin-engine augmentor wing airplane were evaluated in two phases. Design aspects of the over-the-wing/internally blown flap hybrid, augmentor wing, and mechanical flap aircraft were investigated for 910 m. field length with parametric extension to other field lengths. Fuel savings achievable by application of advanced lift concepts to short-haul aircraft were evaluated and the effect of different field lengths, cruise requirements, and noise levels on fuel consumption and airplane economics at higher fuel prices were determined. Conclusions and recommendations are presented.</p></blockquote><p></p><p><a href="http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012219_1975012219.pdf">http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012219_1975012219.pdf</a></p><p></p><p>Three-view drawing (top) of 910 m (3000 ft) OTW-IBF vehicle.</p><p></p><p>Three-view drawing (second) of 910 m (3000 ft) OTW-IBF vehicle optimized for DOC2.</p><p></p><p>Three-view drawing (three) of 910 m (3000 ft) AW vehicle optimized for DOC1.</p></blockquote><p></p>
[QUOTE="Triton, post: 77663, member: 3324"] Renshaw, J. H.; [i]et al[/i]. [i]Evaluation of Advanced Lift Concepts and Fuel Conservative Short-Haul Aircraft, Volume 1 [/i] Lockheed Aircraft Corporation June 1974 [quote]The performance and economics of a twin-engine augmentor wing airplane were evaluated in two phases. Design aspects of the over-the-wing/internally blown flap hybrid, augmentor wing, and mechanical flap aircraft were investigated for 910 m. field length with parametric extension to other field lengths. Fuel savings achievable by application of advanced lift concepts to short-haul aircraft were evaluated and the effect of different field lengths, cruise requirements, and noise levels on fuel consumption and airplane economics at higher fuel prices were determined. Conclusions and recommendations are presented.[/quote] [url=http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012219_1975012219.pdf]http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012219_1975012219.pdf[/url] Three-view drawing (top) of 910 m (3000 ft) OTW-IBF vehicle. Three-view drawing (second) of 910 m (3000 ft) OTW-IBF vehicle optimized for DOC2. Three-view drawing (three) of 910 m (3000 ft) AW vehicle optimized for DOC1. [/QUOTE]
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