Frederico Dias Paulino da Costa, A. Gaitonde, Dorian P. Jones
{"title":"Virtual Experiments of Light and Shock Wave Interaction Using Nonlinear Ray Tracing and Photon Mapping","authors":"Frederico Dias Paulino da Costa, A. Gaitonde, Dorian P. Jones","doi":"10.2514/6.2021-1483","DOIUrl":"https://doi.org/10.2514/6.2021-1483","url":null,"abstract":"Light impinging on an aircraft wing surface interacts with the shock waves that form around it due to the high-speed flow and produces an oscillatory optical phenomenon composed of image distortions or shadow patterns, visible from the airborne perspective under particular observer, vehicle operation and illumination conditions. Analogously to traditional experimental techniques of shock wave visualization, the phenomenon can in principle be replicated computationally in its entirety, although the exact conditions that make it visible are still unknown. From a virtual experiment, it remains to be established what can be inferred about the shock wave and the trans-super sonic flow itself from the observed visual artifacts. This paper develops a three-dimensional nonlinear ray equation solver to predict the light propagation from the sun, through the refractive inhomogeneous density field acquired from a two-dimensional computational fluid dynamics (CFD) simulation and assembled as a pseudo-three-dimensional flow domain, to the physically-based reflective wing surface. Employing the traditional linear ray tracing algorithm, the photon mapping rendering technique and a simplified viewing system implementation, this computational tool is then used to assess the differences in the scene illumination caused by the shock wave. The contrast between the reflected radiance values, represented as a color triplet in the RGB space, considering the aerodynamic inhomogeneous flow field and a fictitious homogeneous optical medium demonstrates that the shock wave indeed induces radiometric disturbances. A strategically positioned and oriented recording film is able to capture magnified deflections of light rays and samples of the density of photons result in the reproduction of the shock wave’s shadow formation. Visualized as in the shadowgraphy experiment or observed from a perspective around the aircraft wing, the characteristics of the shadow pattern depend on the number of photons and the direction that they are emitted from the light source.","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"236 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132069706","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
K. Ackerman, I. Gregory, Evangelos A. Theodorou, N. Hovakimyan
{"title":"A Model Predictive Control Approach for In-Flight Acoustic Constraint Compliance","authors":"K. Ackerman, I. Gregory, Evangelos A. Theodorou, N. Hovakimyan","doi":"10.2514/6.2021-1958","DOIUrl":"https://doi.org/10.2514/6.2021-1958","url":null,"abstract":"Vehicle noise remains one of the major barriers to public acceptance of Urban Air Mobility-class aircraft. This work focuses on motion planning for aircraft in noise-sensitive areas","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115339094","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fabian Dettenrieder, Bryson T. Sullivan, Antonio Giovanni Schöneich, S. Laurence, D. Bodony
{"title":"Direct Numerical Simulation of Boundary Layer Receptivity to Acoustic Radiation in a Hypersonic Compression Ramp Flow","authors":"Fabian Dettenrieder, Bryson T. Sullivan, Antonio Giovanni Schöneich, S. Laurence, D. Bodony","doi":"10.2514/6.2021-0368","DOIUrl":"https://doi.org/10.2514/6.2021-0368","url":null,"abstract":"","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129323594","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Development of UCAV Fleet Autonomy by Reinforcement Learning in a Wargame Simulation Environment","authors":"B. Yuksek, Umut M. Demirezen, G. Inalhan","doi":"10.2514/6.2021-0175","DOIUrl":"https://doi.org/10.2514/6.2021-0175","url":null,"abstract":"In this study, we develop a machine learning based fleet autonomy for Unmanned Combat Aerial Vehicles (UCAVs) utilizing a synthetic simulation-based wargame environment. Air-craft survivability is modeled as Markov processes. Mission success metrics are developed to introduce collision avoidance and survival probability of the fleet. Flight path planning is performed utilizing the proximal policy optimization (PPO) based reinforcement learning method to obtain attack patterns with a multi-objective mission success criteria corresponding to the mission success metrics. Performance of the proposed system is evaluated by utilizing the Monte Carlo analysis in which a wider initial position interval is used when compared to the defined interval in the training phase. This provides a preliminary insight about the generalization ability of the RL agent.","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"12 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126940486","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
P. S. Heaney, F. Soranna, M. Sekula, David J. Piatak, James M. Ramey
{"title":"Analysis of Transonic Unsteady Aerodynamic Environments using Unsteady Pressure Sensitive Paint for the Space Launch System Block 1 Cargo Launch Vehicle","authors":"P. S. Heaney, F. Soranna, M. Sekula, David J. Piatak, James M. Ramey","doi":"10.2514/6.2021-1833","DOIUrl":"https://doi.org/10.2514/6.2021-1833","url":null,"abstract":"Predicting launch vehicle unsteady aerodynamic loads due to buffet remains a significant challenge. Current practices for modeling buffet environments involve the development of buffet forcing functions using discrete unsteady pressure measurements acquired during wind-tunnel tests. These practices often result in significant uncertainty in buffet environments for coupled loads analyses due to the complex spatio-temporal nature of the unsteady pressure field and the challenge of its estimation using discrete sensors. Unsteady pressure sensitive paint, on the other hand, can provide unsteady pressure data at a comparatively high spatial density and may overcome the challenge of unsteady pressure field estimation with discrete sensors and lead to improvements in the development of buffet forcing functions. In this paper, comparisons of the fluctuating pressure field are made for the Space Launch System Block 1 cargo launch vehicle measured using unsteady pressure sensitive paint and pressure transducers.","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"65 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132497724","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Adaptive Control for Nonlinear Time-Varying Rotational Systems","authors":"John K. Zelina, Richard Prazenica, T. Henderson","doi":"10.2514/6.2021-1120","DOIUrl":"https://doi.org/10.2514/6.2021-1120","url":null,"abstract":"","PeriodicalId":165313,"journal":{"name":"AIAA Scitech 2021 Forum","volume":"16 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2021-01-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130511550","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}