Mechanical and Aerospace Engineering
Permanent URI for this collectionhttps://hdl.handle.net/20.500.14540/17055
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Item Vibration Analysis of Euro 6 Diesel Engine: A Multidomain and Machine Learning Approach on Sensor Fault(I.O.E, 2026-04) Sharma, Dipak; paudel laxmanItem Comparative Analysis of HVAC Load, Energy Consumption and Cost for a Commercial Building with Different Wall and Roof Insulation Using HAP(I.O.E, 2026-04) Shah, Krishna Dev; amatya, vishwa prasannaItem Design and Fabrication of a Distillation Apparatus for Traditional Alcohol Micro-distilleries(Pulchowk Campus, 2025-03-12) Saud,Sachin; Pahari,Sanjiv; Basnet,Saroj; Ghimire,Madan; Amatya,Vishwa PrasannaNepali traditional liquor ‘Raksi’ is a culturally significant alcoholic beverage predominantly composed of ethanol. Traditionally, it is prepared using crude distillation equipment, which are likely to induce inefficiency, inconsistent quality, and presence of poisonous impurities such as methanol and amyl alcoholItem Development and Bench-Top Validation of Active Ankle-Foot Prosthesis(I.O.E, 2025-03) Shrestha, Bipin; Kunwar, Sandip et al; Bhattrai, NawrajItem Experimental study of leading-edge sinusoidal tubercles on NASA 63215 wing at low reynolds number(I.O.E, 2025-04) Khadka, Bishowdip; Maharjan, Lujaa; Saud, Pradeep; Timalsina, Sewak; Dahal, ChiranjiviItem Flow visualization in centrifugal pump impeller using Particle Image Velocimetry (PIV)(I.O.E, 2025-04) KHANAL, ABLE; GARTAULA, ANUNAYA; DHAKAL, BENZEENA; DHUNGANA, NRIPESH; Shrestha, RajendraItem NUMERICAL AND EXPERIMENTAL STUDY OF FLUIDIC THRUST VECTORING IN A CONVERGING-DIVERGING NOZZLE USING SHOCK VECTOR CONTROL(I.O.E, 2025-03) Shakya, Osika; Kunwar, Rashu; Shrestha, Shreyas et al; Darlami, KamalItem DEVELOPMENT OF AN AUTONOMOUS UNMANNED AERIAL SYSTEM FOR RF SOURCE LOCALIZATION FOR STATIC TARGET(I.O.E, 2025-03) Khadga, Gautam Kumar; Ray, Kunal; Basnet, Madhusudhan et al; Jha, Arun BikramItem BREAST CANCER DETECTION USING MICRO STRIP PATCH ANTENNA(I.O.E, 2025-03) Yadav, Brajesh; Kuwar, Rabin Jung; Bajracharya, Ram Raj; Kafle, Saurav; Jha, Ajay KumarItem FABRICATION, STRUCTURAL INTEGRITY, AND DYNAMIC RESPONSE OF A CARBON FIBER WING WITH STUDY ON MATERIAL PROPERTIES AND VIBRATION CHARACTERIZATION(I.O.E, 2025-03) Shrestha, Bikesh; Karki, Gaurav Jung; Shrestha, Manish; Parajuli, Utsav; Adhikari, Surya PrasadItem DEVELOPMENT OF AUTONOMOUS NAVIGATION ROBOT IN OUTDOOR ENVIRONMENTS USING SLAM TOOLBOX AND NAV2(I.O.E, 2025-03) Poudel, Balkrishna; Khatiwada, Biswash; Bhatta, Manoj; Chhetri, Susil; Poudel, LaxmanItem Simulation and Real Time Implementation of Visual SLAM in an Indoor Environment using a Quadcopter(I.O.E, 2025-03) Shah, Anil Kumar; Yonzan, Bibek; Jayswal, Lucky Babu; Khadka, Samim; Bhattarai, NawrajItem FINAL YEAR PROJECT REPORT ON "EARTHQUAKE RESISTANT DESIGN OF EIGHT STOREY APARTMENT BUILDING"(I.O.E, 2025-04) Khatiwada, Alish; Jha, Avinash; Dulal, Bhupendra; Pandeya, Bibek et al; Bastola, SubashItem Design and Experiment of Negative-Stiffness Electromagnetic Spring for Low-Frequency Vibration Isolation(I.O.E, 2025-03) Subedi, Aayush; Rijal, Rachit; Purbey, Ravin Kumar; Shrestha, Tulsi Narayan; Luitel, Mahesh ChandraItem INVESTIGATION OF EFFECT OF PRINTING PARAMETERS AND REINFORCEMENT ON THE MECHANICAL PROPERTIES OF 3D PRINTED POLYLACTIC ACID (PLA+) COMPOSITES(I.O.E, 2025-03) Karki, Kamal; Niroula, Krishna; Kunwar, Rajeev; Baral, Rejin; Poudel, LaxmanItem Design and Development of a SubsonicWind Tunnel with a Gust Generator Featuring Oscillating Vanes(I.O.E, 2025-03) Khanal, Aayush; Magar, Anjana Thapa; KC, Isha; Kafle, Ishan; Raut, Nischal; Darlami, KamalItem Integrated control system for active fin-controlled rocket stabilization and guidance(I.O.E, 2025-03) Tajpuriya, Manish; Lamichhane, Simonkrith; Paudel, Simran; Lamsal, Sugam; Bhattarai, SudipItem DESIGN AND FABRICATION OF PAD PRINTING MACHINE CAPABLE OF PRINTING IN UNEVEN SURFACE(I.O.E, 2025-05) BHATTARAI, BIBEK; BHANDARI, BIKRAM; KHATRI, AAKASH; CHHETRI, SOHAN; Neupane, SanjayaItem IMPLEMENTATION OF DIGITAL TWIN TECHNOLOGY FOR REAL-TIME MONITORING OF AN AIRCRAFT WING MODEL(I.O.E, 2025-03) Adhikari, Sangam Bahadur; Gandhari, Saphal; Basnet, Suyog; Neupane, Kushal; Shrestha, rajendraItem DESIGN, FABRICATION, AND CHARACTERIZATION OF PISTON DRIVEN SUPERSONIC SHOCK TUBE(I.O.E, 2025-04) Pokharel, Bhawana; Paudel, Jaya; Dhakal, Prajit; Prasar, Prashant Sharma; Bhattrai, SudipA shock tube is a device used to generate and study high-speed shock waves and the phenomena associated with them. This study presents the design, fabrication and characterization of a piston-driven shock tube, a compact and low-cost device designed to produce supersonic flow. The study uses a high-frequency Data Acquisition(DAQ) system comprised of NI X Series USB 6341. The electronics system measures pressure voltage from the transducer, amplifies it, and sends the output to the DAQ system for visualization in LabVIEW. The study utilizes ToF method with a 100 mm transducer spacing for the velocity measurement. A maximum shockwave mach number upto 1.723 was achieved using 0.072mm aluminum diaphragm at maximum burst pressure ratio of 14.239, characterized by x/l ratio. Schlieren imaging is used to visualize the shockwave and flow patterns behind it.