“Two in one” glider concept for unlimited aerobatics and FES-assisted cross-country flying – part 1

Purpose This paper aims to analyze the possibilities and ways of modifying the existing PW-6 glider to obtain its versatile version suitable for unlimited aerobatic and cross-country flight, taking into consideration possible lowering of the cost of the needed modifications regarding the tooling. Moreover, it also aims to estimate the performance that can be achieved through such modifications. Design/methodology/approach The concept of a master load envelope was applied to facilitate the definition of the airframe parts that required strengthening, accounting for various flight missions. MATLAB and the Simulation and Dynamic Stability Analysis (SDSA) package were used to estimate the performances of both full aerobatic and cross-country versions. Computations of necessary aerodynamic characteristics and control derivatives were performed using the PANUKL package. Findings It was shown that the cross-section enlargements were necessary to maintain the airframe strength requirements. Their extent depended on the mission; however, in most cases, the requirements for the full aerobatic version were dimensioning. Furthermore, the required changes were made without tooling redesign, except for the fuselage molds. The estimated performance of the redesigned glider was close to that of a similar two-seater multifunctional glider described in the available literature. Furthermore, the analysis revealed that the implemented modifications haven’t compromised the design from a performance standpoint. Originality/value The results are mainly of a practical importance and can be a guide for designers planning to implement a similar concept. In particular, they indicate aspects that should be analyzed when similar modifications are planned. The use of the “two in one” concept may be of interesting for manufacturers due to the relatively low labor intensity of the product and, consequently, the possibility of offering essentially two different gliders at a cost similar to the cost of one. Moreover, such a concept fits into trend of the sustainable development, especially when the tools modifications are kept to the minor. From the user’s perspective, such a glider can facilitate instructions concerning full aerobatic training and cross-country flying based on thermals.

Authors

Institutions

Publication Details

Journal
Aircraft Engineering and Aerospace Technology
Published
2025-04-04
DOI
https://doi.org/10.1108/aeat-10-2024-0298
Citations
1
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
4.99
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

“Two in one” glider concept for unlimited aerobatics and FES-assisted cross-country flying – part 1

Wojciech Frączek, P. Czarnocki, Jacek Gadomski, Agnieszka Kwiek
1 citations
Aircraft Engineering and Aerospace Technology
Aerospace and Aviation Technology
4.99
article

“Two in one” glider concept for unlimited aerobatics and FES-assisted cross-country flying – part 1

Wojciech Frączek, P. Czarnocki, Jacek Gadomski, Agnieszka Kwiek
article en
1 citations

Abstract

Purpose This paper aims to analyze the possibilities and ways of modifying the existing PW-6 glider to obtain its versatile version suitable for unlimited aerobatic and cross-country flight, taking into consideration possible lowering of the cost of the needed modifications regarding the tooling. Moreover, it also aims to estimate the performance that can be achieved through such modifications. Design/methodology/approach The concept of a master load envelope was applied to facilitate the definition of the airframe parts that required strengthening, accounting for various flight missions. MATLAB and the Simulation and Dynamic Stability Analysis (SDSA) package were used to estimate the performances of both full aerobatic and cross-country versions. Computations of necessary aerodynamic characteristics and control derivatives were performed using the PANUKL package. Findings It was shown that the cross-section enlargements were necessary to maintain the airframe strength requirements. Their extent depended on the mission; however, in most cases, the requirements for the full aerobatic version were dimensioning. Furthermore, the required changes were made without tooling redesign, except for the fuselage molds. The estimated performance of the redesigned glider was close to that of a similar two-seater multifunctional glider described in the available literature. Furthermore, the analysis revealed that the implemented modifications haven’t compromised the design from a performance standpoint. Originality/value The results are mainly of a practical importance and can be a guide for designers planning to implement a similar concept. In particular, they indicate aspects that should be analyzed when similar modifications are planned. The use of the “two in one” concept may be of interesting for manufacturers due to the relatively low labor intensity of the product and, consequently, the possibility of offering essentially two different gliders at a cost similar to the cost of one. Moreover, such a concept fits into trend of the sustainable development, especially when the tools modifications are kept to the minor. From the user’s perspective, such a glider can facilitate instructions concerning full aerobatic training and cross-country flying based on thermals.

Aircraft Engineering and Aerospace TechnologyVol. 97(11)
Warsaw University of Technology (PL)
Openalex Percentile: Top 7%
Aerospace and Aviation Technology
4.99
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.