Deepa Kodali

Dr. Deepa Kodali

Mechanical Engineering, Christian Brothers University, Memphis, Florida, USA
orcid

Research Focus & Metrics

Academic Career Length

11Years (2016-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 December 2020 in Composites Part B: Engineering
Verified
Journal Article
Closed access
CUChibu O. Umerah
Chibu O. Umerah
DKDeepa Kodali
Deepa Kodali
SHSydnei Head
Sydnei Head
SJShaik Jeelani
Shaik Jeelani
Vijaya RangariVijaya Rangari
Vijaya Rangari

16 November 2021 in Journal of Applied Polymer Science
Verified
Journal Article
Open access
PDF file
RMRadhika Mandala
Radhika Mandala
ABAnjaneya Prasad Bannoth
Anjaneya Prasad Bannoth
SASuresh Akella
Suresh Akella
Vijaya RangariVijaya Rangari
Vijaya Rangari
DKDeepa Kodali
Deepa Kodali
Fused deposition modeling (FDM), one among the most commonly used additive manufacturing (AM), techniques has been widely used in recent years to produce customized parts with intricate geometries, especially from thermoplastics. This method was limited in its ability to produce parts for industrial applications due to inferior properties and the poor quality of fabricated parts. Hence, researchers are being driven to discover novel materials that are viable for FDM in order to keep up with enormous demand for functional products. In the recent years, it is widely recognized that the emphasis was placed on the bio‐based polymer composite matrices rather than conventional thermoplastics due to its vital advantages that aid in the replacement of synthetic and perilous materials. On this context, this review focuses on the recent advancements in FDM printing with biomaterials. Specifically, attempts have been made to investigate and provide nutshell of 3D printing of current bio‐based nanocomposites which consist of either bio‐derived filler or polymer matrices in order to make 3D printing sustainable. The effect of fillers on the filaments and FDM based products, evolution of novel characteristics of bio nanocomposites, the printability of the developed composites and their development in leading applications were also investigated and summarized.

Verified
Journal Article
Open access
PDF file
RMRADHIKA MANDALA
RADHIKA MANDALA
GHGurumurthy Hegde
Gurumurthy Hegde
DKDeepa Kodali
Deepa Kodali
VKVenkateswara Rao Kode
Venkateswara Rao Kode
Peanut-shell-based polymer composites have gained significant attention as sustainable and cost-effective materials with potential applications as food packaging films, ceiling tiles, insulation panels, supercapacitors, and electrodes in various industries like the packaging industry, construction, furniture, and electronics. This review article presents a systematic roadmap of the mechanical properties of peanut-shell-based polymer composites, analyzing the influence of factors such as filler content, surface modification techniques, interfacial adhesion, and processing methods. Through an extensive literature review, we highlight the mechanical properties of peanut-shell-based polymer composites. Furthermore, challenges and ongoing research efforts in this field are discussed. This comprehensive review provides valuable insights for researchers, industry professionals, and policymakers, promoting the development and utilization of peanut-shell-based polymer composites for various applications.

1 January 2018 in AIAA Journal
Verified
Journal Article
Closed access
CKChang-Kwon Kang
Chang-Kwon Kang
JCJacob Cranford
Jacob Cranford
MSMadhu K. Sridhar
Madhu K. Sridhar
DKDeepa Kodali
Deepa Kodali
DLDavid Brian Landrum
David Brian Landrum
NSNathan Slegers
Nathan Slegers
An optical tracking facility was used to record the free flight of the Monarch butterfly for a large number of sequential flaps. The system automatically tracked reflective markers, which were modified to reduce the effects of additional mass on the flight characteristics. Measurements were analyzed over 75 flights of 9 butterflies in a climbing trajectory covering a large range of climbing rates. The flapping frequency remained fairly constant at 9.8 Hz. The peak-to-peak flapping amplitude varied more significantly with an average of 246.4°. The phase offset between flapping and body undulation averaged 89°. The body oscillation amplitude was 4.9 mm. Simulations using Theodorsen’s equation coupled with a single mass dynamics equation resulted in a body motion that closely agreed with the observed data. The undulation amplitude increased with the flapping amplitude, but decreased with wing loading. Butterflies have the lowest wing loading among insects, consistent with their large body undulation amplitudes. The wing–body phase offset solely depends on the reduced frequency, a consequence of the timing between the noncirculatory and circulatory forces. These results suggest that this novel experimental framework can increase our understanding of biological flight and development of micro flapping robots.

1 April 2025 in Journal of Magnesium and Alloys
Verified
Journal Article
Open access
JBJalumedi Babu
Jalumedi Babu
AMAnjaiah Madarapu
Anjaiah Madarapu
DKDeepa Kodali
Deepa Kodali
MRM. Venkata Ramana
M. Venkata Ramana

22 November 2017 in Journal of The Royal Society Interface
Verified
Journal Article
Closed access
PDF file
DKDeepa Kodali
Deepa Kodali
CMCory Medina
Cory Medina
CKChang-kwon Kang
Chang-kwon Kang
Hikaru AonoHikaru Aono
Hikaru Aono
Flying animals possess flexible wings that deform during flight. The chordwise flexibility alters the wing shape, affecting the effective angle of attack and hence the surrounding aerodynamics. However, the effects of spanwise flexibility on the locomotion are inadequately understood. Here, we present a two-way coupled aeroelastic model of a plunging spanwise flexible wing. The aerodynamics is modelled with a two-dimensional, unsteady, incompressible potential flow model, evaluated at each spanwise location of the wing. The two-way coupling is realized by considering the transverse displacement as the effective plunge under the dynamic balance of wing inertia, elastic restoring force and aerodynamic force. The thrust is a result of the competition between the enhancement due to wing deformation and induced drag. The results for a purely plunging spanwise flexible wing agree well with experimental and high-fidelity numerical results from the literature. Our analysis suggests that the wing aspect ratio of the abstracted passerine and goose models corresponds to the optimal aeroelastic response, generating the highest thrust while minimizing the power required to flap the wings. At these optimal aspect ratios, the flapping frequency is near the first spanwise natural frequency of the wing, suggesting that these birds may benefit from the resonance to generate thrust.