Aerodynamic Efficiency Enhancements for Air Vehicles, Phase I

The need for aerodynamics-based efficiency enhancements for air vehicles is presented. Concepts are presented for morphing aircraft, to enable the aircraft to optimize its configuration for various flight regimes. Using simulations, wind tunnel testing, and benchtop hardware development, the feasibility of the concepts will be established in Phase I. In Phase II, flight testing will be performed to refine and finalize the designs. The concepts involve tailoring of the wing using adaptive surfaces to acheive drag reduction. This translates to benefits in range, endurance, manueuvering and speed characteristics of the air vehicle.

Data and Resources

Field Value
accessLevel public
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identifier TECHPORT_9997
issued 2006-01-01
landingPage https://techport.nasa.gov/view/9997
modified 2020-01-29
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  • amerigeoss
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  • north-america
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metadata_created 2025-11-22T15:42:28.730723
metadata_modified 2025-11-22T15:42:28.730727
notes The need for aerodynamics-based efficiency enhancements for air vehicles is presented. Concepts are presented for morphing aircraft, to enable the aircraft to optimize its configuration for various flight regimes. Using simulations, wind tunnel testing, and benchtop hardware development, the feasibility of the concepts will be established in Phase I. In Phase II, flight testing will be performed to refine and finalize the designs. The concepts involve tailoring of the wing using adaptive surfaces to acheive drag reduction. This translates to benefits in range, endurance, manueuvering and speed characteristics of the air vehicle.
num_resources 4
num_tags 10
title Aerodynamic Efficiency Enhancements for Air Vehicles, Phase I