System Identification for Propellers at High Incidence Angles-Reference-Cited by-同舟云学术

System Identification for Propellers at High Incidence Angles

Published:2021-11 Issue:6 Volume:58 Page:1336-1350
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Simmons Benjamin M.¹^ORCID

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036329

Reference31 articles.

1. A survey of hybrid Unmanned Aerial Vehicles

2. GeutherS. C.NorthD. D.BusanR. C. “Investigation of a Tandem Tilt-Wing VTOL Aircraft in the NASA Langley 12-Foot Low-Speed Tunnel,” NASA TM-2020-5003178, June 2020.

3. McSwainR. G.GeutherS. C.HowlandG.PattersonM. D.WhitesideS. K.NorthD. D. “An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed,” NASA TM-2020-220437, Jan. 2020.

Cited by 17 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. Experimental Characterization of an Electric Ducted Fan for the SUSAN 25% Scale Research Vehicle;AIAA SCITECH 2024 Forum;2024-01-04

2. Identification of a Stochastic Dynamic Model for Aircraft Flight Attitude Based on Measured Data;International Journal of Aerospace Engineering;2023-10-28

3. Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data;Journal of Aircraft;2023-08-25

4. System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data;Journal of Aircraft;2023-07

5. Identification of an Electric UAV Propulsion System in Icing Conditions;SAE Technical Paper Series;2023-06-15