Design Guide for Pitch-up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing-aspect-ratio Variations [with List of References]

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DESIGN GUIDE FOR PITCH-UP EVALUATION AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS

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Monthly Catalog of United States Government Publications

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LIST OF SELECTED REFERENCES ON NASA PROGRAMS. PREPARED ...BY THE SCIENCE AND TECHNOLOGY DIV. OF THE LIBRARY OF CONGRESS

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List of Selected References on NASA Programs

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Recent Design Studies Directed Towards Elimination of Pitch-up

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Investigation at High Subsonic Speeds of the Use of Low Auxiliary Tail Surfaces Having Dihedral to Improve the Longitudinal and Directional Stability of a T-tail Model at High Lift

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Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings

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Low-speed Pitching Derivatives of Low-aspect-ratio Wings of Triangular and Modified Triangular Plan Forms

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Damping in Pitch of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds

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