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Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft. Volume 2: Summary report of technology aircraft

R. L. Cavage

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Abstract

t Coefficient, L/qS Checkout Control Cubic Double Diameter, In. (0

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t Coefficient, L/qS Checkout Control Cubic Double Diameter, In. (0

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Available abstract

t Coefficient, L/qS Checkout Control Cubic Double Diameter, In. (0

Key concepts: Aeronautics, Cruise, Lift (data mining), Volume (thermodynamics), Aerospace engineering, Engineering, Marine engineering, Computer science

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Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft. Volume 2: Summary report of technology aircraft — Research Paper | ScholarLens

Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft. Volume 2: Summary report of technology aircraft

About this research paper

What this paper is about

Why it matters

Key contribution

Method / approach

Main findings

Limitations

Applications

Available abstract

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