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Verification of sail-flight testing procedures of wing-in-surface effect craft on engineering flight simulator

Jatiningrum D.a, Jenie Y.I.b, Muhammad H.b, Pasaribu H.M.b

a Center for Industrial Technology and System of Transportation, Agency for the Assessment and Application of Technology, Indonesia
b Faculty of Mechanical and Aerospace Engineering, Institute of Technology Bandung, Indonesia

[vc_row][vc_column][vc_row_inner][vc_column_inner][vc_separator css=”.vc_custom_1624529070653{padding-top: 30px !important;padding-bottom: 30px !important;}”][/vc_column_inner][/vc_row_inner][vc_row_inner layout=”boxed”][vc_column_inner width=”3/4″ css=”.vc_custom_1624695412187{border-right-width: 1px !important;border-right-color: #dddddd !important;border-right-style: solid !important;border-radius: 1px !important;}”][vc_empty_space][megatron_heading title=”Abstract” size=”size-sm” text_align=”text-left”][vc_column_text]This paper presents subject of Sail-Flight Test Program constructed for the Wing in Surface Effect Craft (WiSE) 8 ‘Undan’, which is conducted on the WiSE Engineering Flight Simulator (WiSE-EFS). This paper discusses the result and evaluation of test data, and compares it with the predicted performance of a WiSE Craft. The program includes: On-water maneuvering test, Take-off and Landing, In- Ground Effect (IGE) cruise, IGE maneuvering, Out-of-Ground Effect (OGE) Cruise and OGE maneuvering. The configurations subjected to variation are the fuel, center of gravity, and the aileron-rudder interconnection system. Several failures are also induced, including engine and flight control system failures. The result and findings, along with the experience in sail-flight testing a WiSE craft, are described in the end of this paper.[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Author keywords” size=”size-sm” text_align=”text-left”][vc_column_text]Center of gravity,Evaluation of test,Flight control,Interconnection systems,Predicted performance,Surface effect,Test program,Testing procedure[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Indexed keywords” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Funding details” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”DOI” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][/vc_column_inner][vc_column_inner width=”1/4″][vc_column_text]Widget Plumx[/vc_column_text][/vc_column_inner][/vc_row_inner][/vc_column][/vc_row][vc_row][vc_column][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][/vc_column][/vc_row]