Aerodynamic Performance and Static Stability Characteristics of Aircraft with Tail-Mounted Propellers-Reference-Cited by-同舟云学术

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Aerodynamic Performance and Static Stability Characteristics of Aircraft with Tail-Mounted Propellers

Published:2021-11-15 Issue: Volume: Page:1-18
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

van Arnhem Nando¹^ORCID,de Vries Reynard¹,Sinnige Tomas¹^ORCID,Vos Roelof¹,Veldhuis Leo L. M.¹^ORCID

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Funder

Horizon 2020 Framework Programme

Cleansky

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036338

Reference77 articles.

1. GoldsmithI. M. “A Study to Define the Research and Technology Requirements for Advanced Turbo/Propfan Transport Aircraft,” NASA CR-166138, 1981.

2. MileyS. J.von LavanteE. “Propeller Propulsion System Integration—State of Technology Survey,” NASA CR-3882, 1985.

3. HagerR. D.VrabelD. “Advanced Turboprop Project,” NASA SP-495, 1988.

4. WhitlowJ. B.SieversG. K. “Fuel Savings Potential of the NASA Advanced Turboprop Program,” NASA TM-83736, 1984.

5. RevellJ. D.TullisR. H. “Fuel Conservation Merits of Advanced Turboprop Transport Aircraft,” NASA CR-152096, 1977.

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