Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow-Reference-Cited by-同舟云学术

Engineering Method to Estimate the Blade Loading of Propellers in Nonuniform Flow

Published:2020-12 Issue:12 Volume:58 Page:5332-5346
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

van Arnhem Nando¹,de Vries Reynard¹,Sinnige Tomas¹,Vos Roelof¹,Eitelberg Georg¹,Veldhuis Leo L. M.¹

Affiliation:

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

Funder

Cleansky

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference47 articles.

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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. YarosS. F.SexstoneM. G.HuebnerL. D.LamarJ. E.McKinleyR. E. Jr.TorresA. O.BurleyC. L.ScottR. C.SmallW. J. “Synergistic Airframe-Propulsion Interactions and Integrations,” NASA TM-1998-207644, 1998.

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