Work

High Advance Ratio Wind Tunnel Testing of a Slowed Mach-scaled Rotor with Full-Wing and Trailing Propeller Lift and Thrust Compounding

Year: 2025

Type: conference-paper

Source: Vertical Flight Society Annual Forum and Technology Display

DOI: 10.4050/f-0081-2025-0343

Authors: Vivek Uppoor, Howard Zheng, Inderjit Chopra

Institution: University of Maryland, College Park

Language: English

Topic: Aerospace and Aviation Technology

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4411952203

FWCI: 2.656

Cites:

Cited by: 1

Related to: 10