Pinned Repositories
CERTIFICATES
In this repository, you can find my certificates.
CLUSTER_ANALYSE_SEGMENTATION_DES_CLIENTS_FR
"CLUSTER ANALYSE for SEGMANTATION DES CLIENTS
it-cert-automation-practice
Google IT Automation with Python Professional Certificate - Practice files
mankarali
My Personal Profile
NACA_AIRFOILS_and_CATIA
The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). The shape of the NACA airfoils is described using a series of digits following the word "NACA". The parameters in the numerical code can be entered into equations to precisely generate the cross-section of the airfoil and calculate its properties.
PROJECTS
In this repository, you can find some projects which are created in CLARUSWAY BOOTCAMP TRAINING.
PYTHON_DIFFERENT_EXAMPLES
You can find many PYTHON examples.
PYTHON_EDABIT_EXAMPLES
You can find spme EDABIT examples
TEST1
This repo will be deleted. Please ignore it.
TRAINING
You can find some files which were created for training
mankarali's Repositories
mankarali/TRAINING
You can find some files which were created for training
mankarali/CERTIFICATES
In this repository, you can find my certificates.
mankarali/PROJECTS
In this repository, you can find some projects which are created in CLARUSWAY BOOTCAMP TRAINING.
mankarali/CLUSTER_ANALYSE_SEGMENTATION_DES_CLIENTS_FR
"CLUSTER ANALYSE for SEGMANTATION DES CLIENTS
mankarali/PYTHON_DIFFERENT_EXAMPLES
You can find many PYTHON examples.
mankarali/PYTHON_EDABIT_EXAMPLES
You can find spme EDABIT examples
mankarali/it-cert-automation-practice
Google IT Automation with Python Professional Certificate - Practice files
mankarali/mankarali
My Personal Profile
mankarali/NACA_AIRFOILS_and_CATIA
The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). The shape of the NACA airfoils is described using a series of digits following the word "NACA". The parameters in the numerical code can be entered into equations to precisely generate the cross-section of the airfoil and calculate its properties.
mankarali/TEST1
This repo will be deleted. Please ignore it.
mankarali/TEST2
Pleasa ignore this repo TEST2. It will be deleted
mankarali/TEST3
This repo is creating to test and it will be deleted. Please ignore it
mankarali/flask-first-app
test
mankarali/flask_deployment
test_02
mankarali/GOOGLE---IT
Introduction to Git and GitHub
mankarali/pycharm_test
mankarali/test
mankarali/testams