<abstract xmlns="http://www.w3.org/1999/xhtml">

Gyroplanes, as ultralight aircraft, are popular transport vehicles recently. Ultralight aircraft flights take place at a low altitude – their noise is not without effect on people and nature. The localization of the sources of noise and a possibility to decrease the noise of an gyroplane are described in this paper. The rules of design and exploitation of gyroplanes do not define the limits of emitted noise.
Gyroplanes are not noisy aircraft vehicles but for their silencing the knowledge about the sources and frequency range of noise is necessary. The goal of the conducted measurement was to determine the gyro-plane noise properties and the noise measurement methods. The evaluation of the noise sources was made by acoustic beamforming and the directional emission with single microphones at various engine speeds.
The supplement of these tests should be the rotor noise measurement but that investigation should be performed on a special stand, on which the rotor propulsion noise would not disturb the measurement.
</abstract>

Drivetrain Noise of The Gyroplane I-28

<abstract xmlns="http://www.w3.org/1999/xhtml">

This article presents selected results of I-31T propulsion tests, obtained in the framework of EU project ESPOSA (Efficient Systems and Propulsion for Small Aircraft). I-31T aircraft, as a testbed, was fitted with 180 kW turboprop engine TP100. The scope of the work include results of ground and in-flight tests of engine compartment cooling suitability. The purpose of the cooling tests was to prove that temperatures of the propulsion components are within limits set by the engine manufacturer for the engine type in the most disadvantageous conditions on the ground and in flight up to aircraft maximum altitude, maximum ambient temperature and after standard engine shutdown. Engine oil cooling is beyond the scope of this work.
</abstract>

Ground and in-Fligh Testing of Cooling Efficiency of Turboprop Engine Compartment

<abstract xmlns="http://www.w3.org/1999/xhtml">

The purpose of this text is to demonstrate an operation of a compressed air system designed for high air flow laboratories and wind tunnels. Development of such air system is a challenge due to unusual requirements (simultaneous supply of several users having different requirements and necessity to provide extremely high flows) which have to be address by means of adequate compressed air storage capacity and sophisticated control system. Each stage of the design process is going to be described, focusing on the selection of air compressors, air receivers and air dryers, followed by an insight into a development of the control system. The air system being described in this paper was successfully implemented at the Institute of Aviation in Warsaw improving the quality of the compressed air supply and simplifying the research planning.
</abstract>

Institute of Theory of Electrical Engineering, Measurement and Information Systems

Faculty of Electrical Engineering, Warsaw University of Technology

Compressed Air Supply and Distribution System for Aviation Laboratories and Wind Tunnels

<abstract xmlns="http://www.w3.org/1999/xhtml">

The article presents assumptions of the one-dimensional model of the ASz-62IR aircraft engine. This model was developed in the AVL BOOST software. The ASz-62IR is a nine cylinder, aircraft engine in a radial configuration. It is produced by the Polish company WSK “PZL-Kalisz” S. A. The model is used for calculating parameters of the fuel stream and the air stream in intake system of the engine, as well as for the analyses of the combustion process and the exhaust flow to the external environment. The model is based on the equations describing the isentropic flow. The geometry of the channels and all parts of the model has been mapped on the basis of empirical measurements of the engine elements. The model assumes indirect injection where the gasoline was used as a fuel with the calorific value of 43.5 MJ/kg. The model assumes a mixture of a stoichiometric ratio of 14.5. This model is only part of the overall the ASz-62IR engine model. After the simulation tests on the full model the obtained results confirmed the correctness of the model used to create the mixture. It was found that the AVL BOOST software is good for the implementation of this type of work.
</abstract>

Thermodynamic Model of the ASZ-62IR Radial Aircraft Engine

<abstract xmlns="http://www.w3.org/1999/xhtml">

The article presents an aerodynamic concept of UAV in the gyrodyne configuration, as a more efficient one than the currently used UAV airframe configuration applied for monitoring tasks of power lines and railway infrastructure. A sample task which is realised by conceptual gyrodyne based on monitoring aerial power lines was characterised and described. The assumed idea of UAV was shown in comparison to the currently used aircraft configuration presented in the introduction. Referring to momentum theory, hover efficiency of the multicopter and the helicopter was evaluated. In relation to the helicopter, an initial draft of the airframe conception accompanied by a description of advantages of the gyrodyne configuration was exposed. Problems related to the gyrodyne configuration were emphasised in the summary.
</abstract>

Department of Fluid Mechanics and Aerodynamics, Mechanical Engineering and Aeronautics

Aerodynamic Concept of the UAV in the Gyrodyne Configuration

<abstract xmlns="http://www.w3.org/1999/xhtml">

The article describes a computational study, using CFD models, of droplet spray dispersal in the wake of a ‘Turbo Kruk’ airplane up to 500 m downstream. The CFD Reynolds-averaged Navier-Stokes (RANS) models use a Lagrangian (droplet phase) and Eulerian (fluid phase) procedure to predict the droplet trajectories trough the turbulent aircraft wake. The methods described in the work have the potential to improve current models for aerial spraying and will help in the development of new spraying procedures. In this study, the CFD models are used to describe the phenomenon of sprays released from atomizers mounted on the plane. A parametric study of the aircraft model examines the effects of crosswind on the aircraft’s vortex structures and the resulting droplet trajectories. The study shows, that such influence is underestimated in the current models. A comparison of the present results to AGDISP predictions is provided.
</abstract>

Design Analysis & Calculation Group, PZL „Warszawa – Okęcie” S.A. Airbus Defence & Space

CFD Analysis of the Fluid Particles Distribution by Means of Aviation Technique

<abstract xmlns="http://www.w3.org/1999/xhtml">

The Active Gurney Flap (AGF) is a small, flat tab cyclically deployed and retracted at lower surface of the rotor blade near its trailing edge. It is expected that the device may improve performance of modern helicopters. The main goal of presented investigations was to develop research methodology and next to use it in studies on phenomena occurring in the flow around helicopter-rotor blades equipped with AGF. Conducted CFD simulations aimed at validation of the developed methodology as well as at significant supplementing and extension of results of experimental research. Simplified sensitivity analysis has been conducted aiming at determination of geometric and motion-control parameters of the AGF, optimal from point of view of helicopter-performance improvement. Fully three-dimensional simulations of the rotor flight aimed at determination of flight conditions, in which the use of Active Gurney Flaps could significantly improve the rotorcraft performance.
</abstract>

Flow Control on Helicopter-Rotor Blades Via Active Gurney Flap

<abstract xmlns="http://www.w3.org/1999/xhtml">

The paper presents results of simulation calculations concerning an influence of stiffness of blade-hub connection on rotor loads and blades deflections in hover, level flight and pull up maneuver. The three versions of rotor are considered with articulated, elastic and stiff connections of blades and hub. The blades with the same distributions of stiffness, mass and the same aerodynamic characteristics are applied for all rotor cases. The rotor loads are calculated applying Runge-Kutta method to solve the equations of motion of deformable blades. According to the Galerkin method, the parameters of blades motion are treated as combination of considered blade bending and torsion eigen modes. The results of calculations indicate for possibility to generate the greater rotor control moments and to improve helicopter maneuverability in the case of applying the non-changed blade of articulated rotor combined with elastic rotor hub.
</abstract>

A Comparison of Helicopter Main Rotor Features Due to Stiffness of Rotor Blade-Hub Connection

<abstract xmlns="http://www.w3.org/1999/xhtml">

The paper demonstrates the feasibility of quantitative flow visualisation methods for investigation of transonic and supersonic flows. Two methods and their application for retrieving compressible flow field properties has been described: Background Oriented Schlieren (BOS) and Particle Image Velocimetry (PIV). Recently introduced BOS technique extends the capabilities of classical Schlieren technique by use of digital image processing and allow to measure density gradients field. In the presented paper a review of applications of BOS technique has been presented. The PIV is well established technique for whole field velocity measurements. This paper presents application of PIV for determination of the shock wave position above airfoil in transonic flow regime. The study showed that application of quantitative flow visualisation techniques allows to gain new insights on the complex phenomenon of supersonic and transonic flow over airfoils like shock-boundary layer interaction and shock induced flow separation.
</abstract>

Quantitative Visualisation of Compressible Flows

<abstract xmlns="http://www.w3.org/1999/xhtml">

In the next article on synthesis of regulations, the authors presented the general legal requirements for rotorcraft, which is limited to US regulations, because the vast majority of world regulations are based on them. The Institute of Aviation in Warsaw has developed requirements concerning the construction and operation of rotorcraft in Poland. These requirements constitute an important contribution to the regulations of the <bold>Civil Aviation Authority</bold> which are in force in the air space of the Republic of Poland. This paper presents the legal situation of rotorcraft and compares the requirements for helicopters and gyroplane. The conclusions highlighted the differences that arise from regulations between helicopters and rotorcraft. The authors have suggested the necessity to separate provisions for the group of windmills, which is implemented in the regulations of the <bold>Civil Aviation Authority</bold>. The presented work is the second of a planned series of publications in which authors intend to bring some of the issues to the reader about the design aspects of aircraft in selected global aviation regulations.
</abstract>

Various Types of The Rotorcraft Design in the Context of Aerospace Regulations

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Transactions on Aerospace Research

Aims&amp;ScopeAbout: History and MissionQuality AssuranceArchiving and IntegrityOpen Access and FeesAdvertising and MarketingPublishing Schedule AIMS &amp; SCOPE Core Focus and Article SelectionThe primary aim of Transactions on Aerospace Research is to serve as a dynamic platform for the advancement and exchange of state-of-the-art knowledge in aerospace research. The journal covers a wide range of topics in aerospace engineering, including but not limited to:  Aerodynamics and Aeroacoustics Avionics Aircraft Performance, Stability, and Control Structural Engineering Aerospace Materials Propulsion Systems Navigation and Guidance Systems Maintenance and Diagnostics Manufacturing Technologies Safety and Reliability Vibrations and Aeroelasticity Additionally, it welcomes contributions from related scientific areas intersecting with aviation and space exploration, including but not limited to the following:  Astrophysics Astronomy Remote Sensing Photogrammetry Atmospheric Sciences Materials Sciences Aviation and Space Law Aviation and Space Economy Aviation and Space Organization Aviation and Space Medicine History of Aviation and Space Technology Aerospace Communication In view of its history, Transactions on Aerospace Research has played a distinctive role in bringing the Eastern European aviation-engineering traditions to a wider global audience, and integrating them into the broader global traditions. However, the journal now has a more global reach. It continuously seeks to foster innovation and to encourage collaboration among researchers from diverse backgrounds, pushing the boundaries of what is considered possible in aerospace technology and science. By highlighting cutting-edge research and facilitating discourse on emerging trends and challenges, Transactions on Aerospace Research aims to be at the forefront of shaping the future of aerospace engineering and contributing significantly to the field's evolution. Transactions on Aerospace Research is an Open Access journal, offering increased visibility and impact for authors' work. We do not charge any article processing charges or other publication fees. This approach aligns with our mission to disseminate cutting-edge research freely and widely. ABOUT Transactions on Aerospace Research is published by the Łukasiewicz Research Network – Institute of Aviation in Warsaw. History and MissionThe Łukasiewicz Research Network – Institute of Aviation in Warsaw, originally established as the Technical Research Institute of Aviation back in 1926, has played a pivotal role in the testing and development of nearly all Polish-designed aircraft. The beginnings of the journal date back to an early series of publications known as “IBTL Reports”. After WWII, the Institute began publishing a research journal in 1956, then known as Transactions of the Institute of Aviation [Prace Instytutu Lotnictwa]. In 2018 the name was changed to the current one, Transactions on Aerospace Research – the new title reflecting our commitment to being a global platform for all scholars in aviation and space sciences. The primary aim of Transactions on Aerospace Research is to serve as a dynamic platform for the advancement and state-of-the-art knowledge in aerospace research. The journal has played a distinctive role in bringing the Eastern European aviation-engineering traditions to a wider global audience, and integrating them into the broader global traditions. However, the journal now has a more global reach. It continuously seeks to foster innovation and to encourage collaboration among researchers from diverse backgrounds, pushing the boundaries of what is considered possible in aerospace technology and science. By highlighting cutting-edge research and facilitating discourse on emerging trends and challenges, Transactions on Aerospace Research aims to be at the forefront of shaping the future of aerospace engineering and contributing significantly to the field's evolution. Under the leadership of Professor Cezary Galiński, Editor in Chief, our journal has consistently been growing in prestige and global reach. Quality AssuranceEach submission undergoes a rigorous double-blind peer-review process, ensuring the highest standards of academic excellence. We are proud to be indexed in a number of research databases, including the ICI Journals Master List and BazTech databases, highlighting our commitment to quality and accessibility in scientific publishing. Archiving and IntegrityAs a forward-looking scientific journal, we strive to ensure the longevity and integrity of our publications. We utilize the Sciendo archiving system in Portico [https://www.portico.org/] for long-term digital preservation. Additionally, our participation in the Similarity Check System guarantees the originality and trustworthiness of the content we publish. Open Access and Fees Transactions on Aerospace Research is an Open Access journal, offering increased visibility and impact for authors' work. We do not charge any article processing charges or other publication fees. This approach aligns with our mission to disseminate cutting-edge research freely and widely. The publishing costs for the journal are primarily covered by the Scientific Publications Department of the Łukasiewicz Research Network – Institute of Aviation in Warsaw, with additional funding sourced from the Polish Ministry of Education. Advertising and MarketingThe journal does not host any commercial advertising or marketing activities. Publishing ScheduleThe journal is published four times each year: in the months of March, June, September and December. WERSJA PLCELE I ZAKRESOPIS: Historia i misjaZapewnienie jakościArchiwizacja i integralnośćOtwarty dostęp i opłatyReklama i marketingHarmonogram wydawniczy CELE I ZAKRES Główny cel i zakres tematycznyCzasopismo Transactions on Aerospace Research ma za zadanie służyć jako dynamiczna platforma dla rozwoju i wymiany najnowocześniejszej wiedzy w dziedzinie badań nad lotnictwem i kosmonautyką. Czasopismo obejmuje szeroki zakres tematów z dziedziny inżynierii lotniczej i kosmicznej, w tym między innymi:  Aerodynamika i aeroakustyka Awionika Osiągi, stabilność i kontrola statków powietrznych Inżynieria strukturalna Materiały lotnicze i kosmiczne Systemy napędowe Systemy nawigacji i naprowadzania Konserwacja i diagnostyka Technologie produkcyjne Bezpieczeństwo i niezawodność Drgania i aeroelastyczność Ponadto, mile widziane są wypowiedzi z pokrewnych dziedzin naukowych, które przecinają się z lotnictwem i eksploracją kosmosu, w tym między innymi z następujących:  Astrofizyka Astronomia Teledetekcja Fotogrametria Nauki o atmosferze Nauki o materiałach Prawo lotnicze i kosmiczne Lotnictwo i gospodarka kosmiczna Organizacja lotnictwa i przestrzeni kosmicznej Medycyna lotnicza i kosmiczna Historia lotnictwa i technologii kosmicznych Komunikacja lotnicza Ze względu na swoją historię, Transactions on Aerospace Research odgrywa wyróżniającą się rolę w przybliżaniu wschodnioeuropejskich tradycji inżynierii lotniczej szerszej globalnej publiczności i integrowaniu ich z szerszymi tradycjami światowymi. Obecnie czasopismo ma jeszcze bardziej globalny zasięg. Nieustannie dąży do wspierania innowacji i zachęcania do współpracy naukowców z różnych środowisk, przesuwając granice tego, co uważa się za możliwe w technologii lotniczej i nauce. Transactions on Aerospace Research stara się być liderem w kształtowaniu przyszłości inżynierii lotniczej i kosmicznej oraz znacząco przyczyniać się do ewolucji tej dziedziny poprzez podkreślanie najnowocześniejszych badań i ułatwianie dyskusji na temat pojawiających się trendów i wyzwań. Transactions on Aerospace Research jest czasopismem Open Access. Nie pobieramy żadnych opłat za przetwarzanie artykułów ani innych opłat za publikację. Takie podejście jest zgodne z naszą misją swobodnego i szerokiego rozpowszechniania najnowszych badań. OPIS „Transactions on Aerospace Research” jest czasopismo naukowe publikowane przez Sieć Badawczą Łukasiewicz - Instytut Lotnictwa w Warszawie. Historia i misja Sieć Badawcza Łukasiewicz - Instytut Lotnictwa w Warszawie została pierwotnie założona jako Techniczne Zakłady Naukowe Lotnictwa w 1926 roku i odegrała kluczową rolę w testowaniu i rozwoju niemal wszystkich samolotów polskiej konstrukcji. Początki czasopisma sięgają wczesnej serii publikacji znanych jako „Raporty IBTL”. Po II wojnie światowej, w 1956 roku, Instytut rozpoczął wydawanie czasopisma naukowego pod nazwą „Prace Instytutu Lotnictwa”. W 2018 roku nazwa została zmieniona na obecną, czyli „Transactions on Aerospace Research", co odzwierciedla nasze zaangażowanie w bycie globalną platformą dla wszystkich naukowców zajmujących się lotnictwem i naukami kosmicznymi. Czasopismo „Transactions on Aerospace Research” ma za zadanie służyć jako dynamiczna platforma dla rozwoju i wymiany najnowszej wiedzy w dziedzinie badań lotniczych. Czasopismo odgrywa wyróżniającą się rolę w przybliżaniu wschodnioeuropejskich tradycji inżynierii lotniczej szerszej globalnej publiczności i integrowaniu ich z szerszymi tradycjami światowymi. Nieustannie dąży do wspierania innowacji i zachęcania do współpracy naukowców z różnych środowisk, przesuwając granice tego, co uważa się za możliwe w technologii lotniczej i nauce. „Transactions on Aerospace Research” stara się być liderem w kształtowaniu przyszłości inżynierii lotniczej i kosmicznej oraz znacząco przyczyniać się do ewolucji tej dziedziny poprzez podkreślanie najnowocześniejszych badań i ułatwianie dyskusji na temat pojawiających się trendów i wyzwań. Pod kierownictwem profesora Cezarego Galińskiego, redaktora naczelnego, nasze czasopismo konsekwentnie zyskuje na prestiżu i globalnym zasięgu. Na podstawie komunikatu Ministra Edukacji i Nauki z dnia 17 lipca 2023 roku za artykuły publikowane na łamach Transactions on Aerospace Research przyznawane jest 20 punktów do dorobku naukowego. Zapewnienie jakościKażda praca złożona do czasopisma przechodzi rygorystyczny proces recenzji „podwójnie ślepej”, zapewniając najwyższe standardy doskonałości akademickiej. Jesteśmy indeksowani w wielu bazach danych badawczych, w tym w bazach danych ICI Journals Master List i BazTech, co podkreśla nasze zaangażowanie w jakość i dostępność publikacji naukowych. Archiwizacja i integralnośćJako przyszłościowe czasopismo naukowe staramy się zapewnić długowieczność i integralność naszych publikacji. Korzystamy z systemu archiwizacji Sciendo w Portico [https://www.portico.org/] w celu długoterminowej ochrony zasobów cyfrowych. Ponadto nasz udział w systemie Similarity Check gwarantuje oryginalność i wiarygodność publikowanych przez nas treści. Otwarty dostęp i opłatyTransactions on Aerospace Research jest czasopismem Open Access, oferującym większą widoczność i wpływ na pracę autorów. Nie pobieramy żadnych opłat za przetwarzanie artykułów ani innych opłat za publikację. Takie podejście jest zgodne z naszą misją swobodnego i szerokiego rozpowszechniania najnowszych badań. Koszty wydawnicze czasopisma pokrywane są głównie przez Dział Wydawnictw Naukowych Sieci Badawczej Łukasiewicz – Instytutu Lotnictwa w Warszawie, a dodatkowe środki pochodzą z Ministerstwa Edukacji Narodowej. Reklama i marketingCzasopismo nie prowadzi żadnych komercyjnych działań reklamowych ani marketingowych. Harmonogram wydawniczyCzasopismo jest publikowane cztery razy w roku, w miesiącach Marzec, Czerwiec, Wrzesień i Grudzień 