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.

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. 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.

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Rapid Aerostructural Optimization of Wing-Propeller Systems;AIAA SCITECH 2024 Forum;2024-01-04

2. Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft;Journal of Aircraft;2023-07

3. Low-order acoustic prediction tool for estimating noise emissions from distributed propeller configurations;AIAA AVIATION 2023 Forum;2023-06-08

4. Experimental Study of the Aerodynamic Noise of a Pair of Pusher-Propellers Installed Over a Wing;AIAA AVIATION 2023 Forum;2023-06-08

5. Tonal Noise Measurements and Simulations of an Over-The-Wing Propeller;AIAA AVIATION 2023 Forum;2023-06-08