Contact Professor Howard Smith
- Tel: +44 (0) 1234 758387
- Email: Howard.Smith@cranfield.ac.uk
Areas of expertise
- Aircraft Design
Background
Professor Howard Smith has particular interests in advanced aircraft configuration design, the design of Unmanned Aerial Vehicles and aircraft static loads analysis. He is a Fellow of the Royal Aeronautical Society, a Senior Member of the American Institute for Aeronautics and Astronautics and a Fellow of the Higher Education Academy. He was recently awarded a Boeing Welliver Faculty Fellowship, a position previously given to only one non-US citizen since 1995.
Current activities
Howard is head of the Aircraft Design Group at Cranfield University. His multidisciplinary team excels at the integration of technologies, such as structures, airframe systems and avionics, to find solutions to aviation related challenges such as the environment, defence and airline operations. He has been responsible for the creation of a wide range of innovative aircraft concept studies.
Howard currently teaches aircraft conceptual design and aircraft loads analysis to graduate students from all over the world. The unique approach to teaching emphasises learning and assessment through immersion in virtual industrial team projects. The scale of the projects initiated is probably unique in the academic world and attracts interest from aerospace manufacturers and operators alike.
Publications
Articles In Journals
- Zammit K, Smith H, Lobo NS & Giannopoulos IK. (2024). Vortex Lattice CFD Application and Modeling Validation for Ground Effect Aircraft. WSEAS TRANSACTIONS ON FLUID MECHANICS, 19
- Kang L, Sun Y, Smith H & Mao J. (2023). The Effects of the Degree of Hybridisation on the Design of Hybrid-Electric Aircraft Considering the Balance between Energy Efficiency and Mass Penalty. Aerospace, 10(2)
- Sun Y & Smith H. (2022). Design and operational assessment of a low-boom low-drag supersonic business jet. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 236(1)
- Kang L, Sun Y & Smith H. (2022). MDAO Method and Optimum Designs of Hybrid-Electric Civil Airliners. Journal of Aerospace Engineering, 35(4)
- Sun Y & Smith H. (2022). Conceptual design of sonic boom stealth supersonic transports. CEAS Aeronautical Journal, 13(2)
- Wei C, Lin G, Huang J, Song L & Smith H. (2022). Flight testing verification of lateral-directional dynamic stability of gliding birds due to wing dihedral. Aircraft Engineering and Aerospace Technology, 94(11)
- RAJENDRAN P & SMITH H. (2020). Experimental Analysis of Small Solar Unmanned Aerial Vehicle to Predict Aerodynamic Performance. INCAS BULLETIN, 12(4)
- Sun Y & Smith H. (2020). Low-boom low-drag solutions through the evaluation of different supersonic business jet concepts. The Aeronautical Journal, 124(1271)
- Sun Y & Smith H. (2019). Low-boom low-drag optimization in a multidisciplinary design analysis optimization environment. Aerospace Science and Technology, 94
- Sepulveda Palacios E & Smith H. (2019). Impact of mission requirements on the design of low observable UCAV configurations. Aircraft Engineering and Aerospace Technology, 91(10)
- Sepulveda E, Smith H & Sziroczak D. (2019). Multidisciplinary analysis of subsonic stealth unmanned combat aerial vehicles. CEAS Aeronautical Journal, 10(2)
- Smith H, Sziroczák D, Abbe GE & Okonkwo P. (2019). The GENUS aircraft conceptual design environment. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233(8)
- Rajendran P & Smith H. (2018). Experimental Assessment of Various Batteries and Propellers for Small Solar-Powered Unmanned Aerial Vehicle. Journal of Engineering and Technological Sciences, 50(3)
- Rajendran P & Smith H. (2018). Development of Design Methodology for a Small Solar-Powered Unmanned Aerial Vehicle. International Journal of Aerospace Engineering, 2018
- Sun Y & Smith H. (2017). Review and prospect of supersonic business jet design. Progress in Aerospace Sciences, 90(April)
- Sepulveda E & Smith H. (2017). Technology challenges of stealth unmanned combat aerial vehicles. The Aeronautical Journal, 121(1243)
- Sziroczak D & Smith H. (2016). A review of design issues specific to hypersonic flight vehicles. Progress in Aerospace Sciences, 84(July)
- Rajendran P & Smith H. (2016). Modelling of solar irradiance and daylight duration for solar-powered UAV sizing. Energy Exploration & Exploitation, 34(2)
- Abbe G & Smith H. (2016). Technological development trends in Solar‐powered Aircraft Systems. Renewable and Sustainable Energy Reviews, 60
- Okonkwo P & Smith H. (2016). Review of evolving trends in blended wing body aircraft design. Progress in Aerospace Sciences, 82
- Rajendran P & Smith H. (2015). Review of Solar and Battery Power System Development for Solar-Powered Electric Unmanned Aerial Vehicles. Advanced Materials Research, 1125
- Rajendran P & Smith H. (2015). Future Trend Analysis on the Design and Performance of Solar-Powered Electric Unmanned Aerial Vehicles. Advanced Materials Research, 1125
- Rajendran P & Smith H. (2015). Implications of longitude and latitude on the size of solar-powered UAV. Energy Conversion and Management, 98
- Manzanera RAJ & Smith H. (2015). Flight in nature I: Take-off in animal flyers. The Aeronautical Journal, 119(1213)
- Fielding JP, Mills A & Smith H. (2010). Design and manufacture of the DEMON unmanned air vehicle demonstrator vehicle. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 224(4)
Conference Papers
- Taflan M, Smith H & Loughlan J. (2023). Parametric Analysis for Structural Design and Weight Estimation of Cantilever and Strut-Braced Wing-Boxes
- Chan JL, Sun Y & Smith H. (2023). Airliner conceptual designs for the application of alternative fuels
- Gao Z & Smith H. (2020). Blended Wing Body with Boundary layer Ingestion Conceptual Design in a Multidisciplinary Design Analysis Optimization Environment
- Smith H & Sun Y. (2020). Design Case of the E-19 AEOLUS Supersonic Business Jet
- Sun Y, Smith H & Chen H. (2020). Conceptual Design of Low-Boom Low-Drag Supersonic Transports
- Sepulveda E & Smith H. (2019). Conceptual design of a fifth generation unmanned strike fighter
- Sun Y & Smith H. (2018). Supersonic Business Jet Conceptual Design in a Multidisciplinary Design Analysis Optimization Environment
- Sun Y & Smith H. (2018). Sonic Boom and Drag Evaluation of Supersonic Jet Concepts
- Rajendran P, Mazlan NM & Smith H. (2017). Single Cell Li-Ion Polymer Battery Charge and Discharge Characterizations for Application on Solar-Powered Unmanned Aerial Vehicle
- Rajendran P & Smith H. (2014). The Development of a Small Solar Powered Electric Unmanned Aerial Vehicle Systems
- Rajendran P, Smith H & bin Masral MH. (2014). Modeling and Simulation of Solar Irradiance and Daylight Duration for a High-Power-Output Solar Module System
- Fielding JP, Stocking P & Smith H. (2010). Comparison of fuel burn and noise characteristics of novel aircraft configurations
- Okonkwo P & Smith H. Packaging in a Multi Conceptual Design Synthesis of a BWB Aircraft
Books
- Smith H. (2012). Innovation in supersonic passenger air travel In Young T & Hirst M (eds), Innovation in Aeronautics. Woodhead Publishing.
- Young TM, Hirst M, Bar-Cohen Y, Guiler RW, Hamburg SD, .... (2012). Contributor contact details In Innovation in Aeronautics. Elsevier.
- Mistry S, Smith H & Fielding JP. (2009). Commercial Aircraft Design for Reduced Noise and Environmental Impact In Buttazzo G & Frediani A (eds), Variational Analysis and Aerospace Engineering (33). Springer New York.