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This case aims to describe what innovation looks like and how it works in Fidelity Investments, a financial services organization that is large and decentralized.

The case looks at how the firm's internal consultants introduced idea‐management systems, idea‐management contests, design thinking, open innovation, innovation tools, coaching and mentoring and new innovation processes

The study show that internal consultants made progress by demonstrating that different ways of thinking through business problems could lead to better solutions without making a huge investment of resources – people, time, and budget.

The implementation results findings are based on first‐hand reporting by the author.

The combination of internal consultants and business unit champions learned to create a home for innovation that focuses and leverages impact.

This case explains how the internal consulting unit charged with disseminating innovation processes developed the trust and cooperation of the company business units.

The purpose of this paper is to present the status of the on-going development of the new computerized environment for aircraft synthesis and integrated optimization methods (CEASIOM) and to compare results of different aerodynamic tools. The concurrent design of aircraft is an extremely interdisciplinary activity incorporating simultaneous consideration of complex, tightly coupled systems, functions and requirements. The design task is to achieve an optimal integration of all components into an efficient, robust and reliable aircraft with high performance that can be manufactured with low technical and financial risks, and has an affordable life-cycle cost.

CEASIOM (www.ceasiom.com) is a framework that integrates discipline-specific tools like computer-aided design, mesh generation, computational fluid dynamics (CFD), stability and control analysis and structural analysis, all for the purpose of aircraft conceptual design.

A new CEASIOM version is under development within EU Project AGILE (www.agile-project.eu), by adopting the CPACS XML data-format for representation of all design data pertaining to the aircraft under development.

Results obtained from different methods have been compared and analyzed. Some differences have been observed; however, they are mainly due to the different physical modelizations that are used by each of these methods.

This paper summarizes the current status of the development of the new CEASIOM software, in particular for the following modules: CPACS file visualizer and editor CPACSupdater (Matlab) Automatic unstructured (Euler) & hybrid (RANS) mesh generation by sumo Multi-fidelity CFD solvers: Digital Datcom (Empirical), Tornado (VLM), Edge-Euler & SU2-Euler, Edge-RANS & SU2-RANS Data fusion tool: aerodynamic coefficients fusion from variable fidelity CFD tools above to compile complete aero-table for flight analysis and simulation.

To obtain a good start configuration in the early design phase, simulation tools are used to create a large number of product designs and to evaluate their performance. To reduce the effort for the model generation, analysis and evaluation, a design environment for thin-walled lightweight structures (DELiS) with the focus on structural mechanics of aircrafts has been developed.

The core of DELiS is a parametric model generator, which creates models of thin-walled lightweight structures for the aircraft preliminary design process. It is based on the common parametric aircraft configuration schema (CPACS), which is an abstract aircraft namespace. DELiS facilitates interfaces to several commercial and non-commercial finite element solvers and sizing tools.

The key principles and the advantages of the DELiS process are illustrated. Also, a convergence study of the finite element model of the wing and the fuselage and the result on the mass after the sizing process are shown. Due to the high flexibility of model generation with different levels of detail and the interface to the exchange database CPACS, DELiS is well suited to study the structural behaviour of different aircraft configurations in a multi-disciplinary design process.

The abstract definition of the object-oriented model allows several dimensions of variability, such as different fidelity levels, for the resulting structural model. Wings and fuselages can be interpreted as finite beam models, to calculate the global dynamic behaviour of a structure, or as finite shell models.

This commentary discusses the paper by Reardon et al. (2024; this issue) entitled, “Overcoming implementation challenges through using a train-the-trainer approach to teach numeracy in a special school setting.” This commentary outlines the necessary contribution this paper adds to the substantive area of research it is couched within while also identifying potential areas of future research to expand the understanding of this phenomenon and its impact upon practice.

What is fidelity of implementation, how do we measure it and how does it impact our interpretations of experimental findings? This commentary focuses specifically on the nebulous construct of fidelity in experimental studies and how this impacts experimental findings’ internal and external validity.

Although fidelity is frequently referenced as an important aspect to consider, the measurement of the construct has been critiqued in experimental studies. To understand if an intervention was “implemented as intended,” the core dimensions of the intervention must be considered in the measurement process, as well as potential confounding variables.

With an increased need for experimental work to inform what works, for whom and under what conditions, there becomes a need to better investigate the implementation of the intervention in these contexts – thus, fidelity must be reconceptualized. This commentary provides an overview of this dilemma with potential ideas to investigate moving forward.

This article reports on three pragmatic randomised controlled trials (RCTs) to help children at risk of conduct disorder (CD): two involved the Incredible Years (IY) BASIC parent programme and the other concerned the IY teacher programme. All three interventions took place in regular service settings in North‐ and Mid‐Wales. In all three studies, staff from the provider agency delivered the programme and participated in RCT evaluations in which participants were randomly allocated to intervention or waitinglist control conditions. After a brief introduction to research into the prevention or treatment of CD, and the issues to be considered by services in selecting and delivering interventions, this article summarises the structure, content and evidence base of the IY programmes. The three Welsh studies are briefly described before exploring what factors contributed to service participation in the trials and the benefits and lessons learned in undertaking them.

There is growing literature on the application of Dialectical Behaviour Therapy (DBT) with adults with intellectual disabilities (IDs). To draw upon the evidence-base from mainstream approaches, adapted interventions must remain true to their theoretical foundations and retain key components. The purpose of this paper was to establish the extent to which DBT has been adapted for adults with ID, and whether existing adapted protocols can still be considered DBT.

The theoretical underpinnings and key components of DBT were identified. Six DBT studies were critiqued according to these criteria.

In terms of content, only one intervention comprised all necessary elements. All of the remaining interventions included a skills group; two included individual therapy and another two included group consultation. None of the remaining interventions provided 24-h telephone support. Furthermore, none of the studies explicitly described using dialectical strategies.

To the best of the authors’ knowledge, this is the first paper to critically examine the evidence-base for the use of DBT in ID, particularly its fidelity.

This paper describes the author's work during 35 years as a clinical psychologist in the NHS in Wales working mainly with conduct disordered children and their families. It describe how from initially working within an applied behaviour analysis (ABA) framework with individual families she subsequently established and researched the group based Incredible Years (IY) parent programme in Wales and led a Wales‐wide dissemination of the IY programmes.

The paper provides a case study example of the use of the Society for Prevention Research (SPR) criteria for translational research, that is research that can be applied successfully in the real world.

Many of the challenges were overcome through the inclusion of strategies to maximise effectiveness with differing populations, and by gaining the support of government and local services.

The paper discusses the challenges of taking an evidence‐based programme to scale.

The purpose of this paper is to present the preliminary design of a medium altitude long endurance (MALE) unmanned aerial vehicle (UAV), focusing on the interaction between the aerodynamic and the structural design studies.

The classic layout theory was used, adjusted for the needs of unmanned aircraft, including aerodynamic calculations, presizing methods and CFD, to estimate key aerodynamic and stability coefficients. Considering the structural aspects, a combination of layout, finite element methods and custom parameterized design tools were used, allowing automatic reshapes of the skin and the internal structural parts, which are mainly made of composite materials. Interaction loops were defined between the aforementioned studies to optimize the performance of the aerial vehicle, maximize the aerodynamic efficiency and reduce the structural weight.

The complete design procedure of a UAV is shown, starting from the final stages of conceptual design, up to the point where the detail design and mechanical drawings initiated.

This paper presents a complete view of a design study of a MALE UAV, which was successfully constructed and flight-tested.

This study presents a complete, synergetic approach between the configuration layout, aerodynamic and structural aspects of a MALE UAV.

A multi-disciplinary robust design optimization method for micro Mars entry probe (no more than 0.8 m in diameter) is proposed. The purpose of this paper is to design a Mars entry probe, not only the geometric configuration, but the trajectory and thermal protection system (TPS). In the design optimization, the uncertainties of atmospheric and aerodynamic parameters are taken into account. The probability distribution information of the uncertainties are supposed to be unknown in the design. To ensure accuracy levels, time-consuming numerical models are coupled in the optimization. Multi-fidelity approach is designed for model management to balance the computational cost and accuracy.

Uncertainties which cannot defined by usual Gaussian probability distribution are modeled with degree of belief, and optimized through with multiple-objective optimization method. The optimization objectives are set to be the thermal performance of the probe TPS and the corresponding belief values. Robust Pareto front is obtained by an improved multi-objective density estimator algorithm. Multi-fidelity management is performed with an Artificial Neural Network (ANN) surrogate model. Analytical model is used first, and then with the improvement of accuracy, rather complex numerical models are activated. ANN updates the database during the optimization, and makes the solutions finally converge to a high-level accuracy.

The optimization method provides a way for conducting complex design optimization involving multi-discipline and multi-fidelity models. Uncertainty effects are analyzed and optimized through multi-disciplinary robust design. Because of the micro size, and uncertain impacts of aerodynamic and atmospheric parameters, simulation results show the performance trade-off by the uncertainties. Therefore an effective robust design is necessary for micro entry probe, particularly when details of model parameter are not available.

The optimization is performed through a new developed multi-objective density estimator algorithm. Affinity propagation algorithm partitions adaptively the samples by passing and analyzing messages between data points. Local principle component techniques are employed to resample and reproduce new individuals in each cluster. A strategy similar to NSGA-II selects data with better performance, and converges to the Pareto front. Models with different fidelity levels are incorporated in the multi-disciplinary design via ANN surrogate model. Database of aerodynamic coefficients is updated in an online manner. The computational time is greatly reduced while keeping nearly the same accuracy level of high fidelity model.

The purpose of this study is to describe the development of the 14-item reflective fostering fidelity rating (RFFR), an observational rating system to evaluate model fidelity of group facilitators in the Reflective Fostering Programme (RFP), a mentalisation-based psychoeducation programme to support foster carers. The authors assess usability, dimensionality, inter-rater reliability and discriminative ability of the RFFR.

Eighty video clip extracts documenting 20 RFP sessions were independently rated by four raters using the RFFR. The dimensionality of the RFFR was assessed using principal components analysis. Inter-rater agreement was assessed using the intra-class correlation coefficient.

The proportion of missing ratings was low at 2.8%. A single principal component summarised over 90% of the variation in ratings for each rater. The inter-rater reliability of individual item ratings was poor-to-moderate, but a summary score had acceptable inter-rater reliability. The authors present evidence that the RFFR can distinguish RFP sessions that differ in treatment fidelity.

To the best of the authors’ knowledge, this is the first investigation and report of the RFFR’s validity in assessing the programme fidelity of the RFP. The paper concludes that the RFFR is an appropriate rating measure for treatment fidelity of the RFP and useful for the purposes of both quality control and supervision.