Back to results

Embry Riddle Aeronautical University

Conceptual Design Methodology for the Fan-in-Wing VTOL Aircraft

Abstract

dc:description.abstract

<p>The Fan-In-Wing (FIW) aircraft concept is one of the most compelling solutions for missions demanding jet-like cruise speeds and Vertical TakeOff and Landing (VTOL) capability. However, despite years of interest and documented improvements in lift-fan technology, there exists little in the way of an adequate theory for conceptual design of a fan-in-wing aircraft. To address this issue, a general conceptual design methodology has been developed as a source of guidance for the FIW designer. Through this work, the top-level requirements ranking the fan-in-wing concept above other VTOL aircraft have been defined, while a cross-comparison between the FIW concept and conventional aircraft reveals major discrepancies in their design philosophies, constituting the need for a separate design algorithm. The final conceptual design methodology emerges from an elaborate technique of relating the FIW concept’s major cruise and hover performance metrics to a physical disk area constraint imposed by the size of its wing reference area. Out of this process, a theoretical and practical design space for sizing the FIW concept has been defined, and as a result, the FIW aircraft designer is given an effective means of iterating on the initial size of their wings and lift fans to meet a set of cruise and hover performance requirements. A final demonstration of how the conceptual FIW design methodology is implemented in practice has been included using an example case study.</p>

Degree

thesis:*
Name thesis:degree_name
Master of Science in Aerospace Engineering
Level thesis:degree_level
Thesis - Open Access
Discipline thesis:degree_discipline
Aerospace Engineering
Year
2024

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Steinfeldt, Brock

Subjects

dc:subject × 12

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/818
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1846

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Steinfeldt, Brock. Conceptual Design Methodology for the Fan-in-Wing VTOL Aircraft. Thesis - Open Access thesis, 2024. https://commons.erau.edu/edt/818