SAWE Technical Papers
Showing 737–752 of 2059 results
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197. Specification for the Standard Presentation of Basic Data Needed by an Airline for Purposes of Weight and Balance Evaluatio
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1971. PDWING – A Preliminary Design Multi-Station Wing Analysis Program
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1972. Titanium Matrix Composite (TMC) Weight Evaluation and Validation
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1974. An Improved Methodology for Estimating Advanced Composite Airframe Weights During Conceptual and Preliminary Design
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1976. Explosively Welded Composites for Radiation Shielding
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198. Possibility of Measuring the Safety Built Into Airline Loading Systems and Assumptions (Outline)
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1981. Automated Assembly of Complex Aircraft Structure
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1983. Ceramic Matrix Composites for Weight Critical Hot Structure
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1984. Advanced Composite Weight Reduction on the MD-11 Aircraft
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1985. Aluminum Alloy Development Efforts for Compression Dominated Structure of Aircraft
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1986. Weight and Accountability – an Airline Point of View
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1989. Aircraft Weighing: A Focal Point in Mass Properties Engineering
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199. One Airline’s Approach to the Load Dispatch Problem
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1990. Average “”Passenger and Hand Baggage Weight Survey””
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1991. Avionics, From Design to the Airline
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1992. Launch Vehicle Synthesis and Methodology
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