Aerodynamic Performance of an Aircraft Equipped with Horizontal Tail Mounted Propellers-Reference-Cited by-同舟云学术

Aerodynamic Performance of an Aircraft Equipped with Horizontal Tail Mounted Propellers

Published:2019-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aviation 2019 Forum
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Author:

van Arnhem Nando¹,de Vries Reynard¹,Vos Roelof¹,Veldhuis Leo L.¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Whitlow, J. B., and Sievers, G. K. “Fuel Savings Potential of the NASA Advanced Turboprop Program,” Tech. Rep. TM-83736, NASA, 1984.

2. Goldsmith, I. M. “A Study to Define the Research and Technology Requirements for Advanced Turbo/Propfan Transport Aircraft,” Tech. Rep. CR-166138, NASA, 1981.

3. Sullivan, W. E., Turnberg, J. E., and Violette, J. A. “Large-Scale Advanced Prop-Fan Blade Design,” Tech. Rep. CR-174790, NASA, 1984.

4. Performance evaluation and DOC Estimation of an Innovative Turboprop Configuration

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