{'fraction_non_alphanumeric': 0.014161220043572984, 'fraction_numerical': 0.0, 'mean_word_length': 4.8164556962025316, 'pattern_counts': {'":': 0, '<': 0, '<?xml version=': 0, '>': 0, 'https://': 0, 'lorem ipsum': 0, 'www.': 0, 'xml': 0}, 'pii_count': 0, 'substrings_counts': 0, 'word_list_counts': {'cursed_substrings.json': 0, 'profanity_word_list.json': 0, 'sexual_word_list.json': 0, 'zh_pornsignals.json': 0}}
Analysis of Buckling and Characteristics in Wings of Aircraft

With increasing technology and demand, most people choose airplanes as traffic tools, so safety is one of the most important parts that need to be guaranteed. At present, most wings of aircraft are made in thin-walled structure of rod plate, this kind of structure can provide greater load capacity, and wings may buckle when load caused by air apply to it. In this way, designers should concern more to involve this kind of issue, by using what kind of composite material that has more load capacity and stronger structure. This article will summarize the general design for airliner in the use of material and structure, will also contain the relationship between the design of wings and reduce buckling with previous research and calculation to analyze the first and second order of buckling that will occur and affect the safety of the whole airplane.