Lockheed Advanced Lift Fuel Conservative Short-Haul Airliner Concepts

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Renshaw, J. H.; et al. Evaluation of Advanced Lift Concepts and Fuel Conservative Short-Haul Aircraft, Volume 1 Lockheed Aircraft Corporation June 1974

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.

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012219_1975012219.pdf

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.

 

[Triton]

Additional concepts from Renshaw, J. H.; et al. Evaluation of Advanced Lift Concepts and Fuel Conservative Short-Haul Aircraft, Volume 1 :

Three-view drawing (top) of MF general arrangement, FPR 1.35.

Three-view drawing (second) of 1220 m (4000 ft) MF vehicle DOC 2.

Three-view drawing (third) of Lockheed powered lift model (high wing)

Three-view drawing (fourth) of Lockheed powered lift model (low wing)

 

[Triton]

Renshaw, J. H.; et al. Evaluation of Advanced Lift Concepts and Fuel Conservative Short-Haul Aircraft, Volume 2 Lockheed Aircraft Corporation June 1, 1974

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012220_1975012220.pdf

 

[jrlucariny]

View: https://youtu.be/fxdnu6a-N4s