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Pre-study example to choose the dimensions of the main wing of an aircraft, according to the specifications (Stall speed, cruise speed and range requirements).<\/p>\n
Features demonstrated in this tutorial:
\n– Draft analysis
\n– Power model for an engine with a constant speed propeller
\n– Fuel consumption model
\n– Mission simulation[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”1637″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto2\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto2%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
VLM study example, how to model an aircraft and its stability.<\/p>\n
Features demonstrated in this tutorial:
\n– VLM geometry modeling
\n– Aerodynamics and sideslip analysis, estimating longitudinal and directional stability
\n– Dynamic stability[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”1960″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto3\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto3%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
2D Navier-Stokes study example, how to model a 2D airfoil with a flap.<\/p>\n
Features demonstrated in this tutorial:
\n– NS 2D geometry modeling
\n– 2D Aerodynamics analysis
\n– Comparative visualisations
\n– Comparative charts[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”2293″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto4\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto4%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
3D Navier-Stokes study example, how to make a basic 3d model of an aicraft and iterate on the design.<\/p>\n
Features demonstrated in this tutorial:
\n– Basics of NS 3D geometry modeling
\n– 3D Aerodynamics analysis
\n– Managing runs in the queue
\n– Estimating a good position for static ports[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”2294″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto5\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto5%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
3D Navier-Stokes study example, how to make a 3d model with controls of an aicraft. Then investigating the stall speed in a landing configuration and as well as the CoG range.<\/p>\n
Features demonstrated in this tutorial:
\n– Setting up rotating and shifting parts
\n– Checking the stall speed in a landing configuration
\n– Finding the aft limit of the CoG
\n– Finding the forward limit of the CoG[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”2428″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto6\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto6%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
3D Navier-Stokes study example, how to model undercowl flows to optimise engine cooling.<\/p>\n
Features demonstrated in this tutorial:
\n– Setting up custom refinements in geometries
\n– Setting up a rotor model in a Navier-Stokes computation
\n– Setting up engine air intake and exhaust.
\n– Setting up a liquid-to-air heat exchanger in a Navier-Stokes computation
\n– Estimating variation of cooling on air-cooled engine cylinders, using skin friction reports.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”2491″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto7\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto7%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
3D Navier-Stokes study example, how to model VTOL to horizontal flight transition.<\/p>\n
Features demonstrated in this tutorial:
\n– Using refinement volumes.
\n– Modeling rotors with custom coefficients.
\n– Modeling hovering flight.
\n– Checking the aerodynamics and rotors forces and moments.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner css=”.vc_custom_1650353590777{padding-bottom: 40px !important;}”][vc_column_inner width=”1\/4″ css=”.vc_custom_1650353955834{padding-top: 20px !important;}”][vc_single_image image=”2513″ img_size=”medium” onclick=”custom_link” img_link_target=”_blank” link=”https:\/\/aceofaircraft.aero-ce.com\/tutorials\/tuto7\/tuto.html”][vc_btn title=”Open tutorial” style=”classic” color=”primary” link=”url:https%3A%2F%2Faceofaircraft.aero-ce.com%2Ftutorials%2Ftuto8%2Ftuto.html||target:%20_blank|”][\/vc_column_inner][vc_column_inner width=”3\/4″][vc_column_text]<\/p>\n
3D Navier-Stokes and VLM study example, how to estimate the stability derivatives of an aircraft.<\/p>\n
Features demonstrated in this tutorial:
\n– estimation of the stability derivatives for an alpha or beta change (with NS)
\n– estimation of the derivatives for each axis turning rate. (Pitch\/Yaw\/Roll damping) (with NS)
\n– same computations but with the VLM solver for comparison.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][\/vc_column][\/vc_row]<\/p>\n","protected":false},"excerpt":{"rendered":"
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