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Application of Metallic Materials for Aircraft Structures in the Temperature Range 600 to 1100 F

Published 1956-01-01 by SAE International in United States
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THE SYNTHESIS OF AIRCRAFT HYDRAULIC SERVOS

Published 1956-01-01 by SAE International in United States
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High-Temperature Problems Associated with the Use of Rubber in Aircraft

Published 1956-01-01 by SAE International in United States
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Mach 3 Wing Structures Stiffened Skin versus Sandwich

Published 1961-01-01 by SAE International in United States
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A Design Description Of The Navion

Published 1947-01-01 by SAE International in United States
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Implications of Re-Entry Trajectory Control on Vehicle Design Criteria at Superorbital Speeds

Published 1962-01-01 by SAE International in United States
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Graphic PERT/Cost Milestone Reporting

Published 1962-01-01 by SAE International in United States
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PROBLEMS ASSOCIATED WITH THE MANUFACTURING OF RADOMES

Published 1952-01-01 by SAE International in United States
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Three Explosive Applications to Metal Forming

Published 1964-01-01 by SAE International in United States
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Remote Measurement of Differential Atmospheric Velocity

Published 1966-02-01 by SAE International in United States
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