Static Stability Characteristics of a Manned Lifting Entry Vehicle at High Subsonic Speeds
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Published: 1967
Total Pages: 162
ISBN-13:
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Author:
Publisher:
Published: 1967
Total Pages: 162
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DOWNLOAD EBOOKAuthor: George M. Ware
Publisher:
Published: 1967
Total Pages: 46
ISBN-13:
DOWNLOAD EBOOKAn investigation has been made of the low-subsonic flight characteristics of a model of the HL-10 manned lifting entry vehicle. This model was tested with two different center fins and with the larger center fin in combination with fin tips.
Author: Robert W. Kempel
Publisher:
Published: 1994
Total Pages: 60
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DOWNLOAD EBOOKAuthor: Joseph R. Chambers
Publisher:
Published: 1967
Total Pages: 76
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DOWNLOAD EBOOKAn analytical investigation has been made to determine the dynamic longitudinal and lateral stability and response of the HL-10 entry vehicle with particular reference to low-speed, high-angle-of-attack conditions. The calculations were made for light and heavy wing loadings for both sea level altitude flight. The results indicate that the HL-10 vehicle was dynamically longitudinally and laterally stable for the conditions investigated but that artificial damping in pitch and roll was required for some conditions in order to achieve a satisfactory degree of stability based on military handling qualities specifications for piloted airplanes.
Author: Robert F. Stengel
Publisher: Princeton University Press
Published: 2004-10-17
Total Pages: 863
ISBN-13: 0691114072
DOWNLOAD EBOOKFlight Dynamics takes a new approach to the science and mathematics of aircraft flight, unifying principles of aeronautics with contemporary systems analysis. While presenting traditional material that is critical to understanding aircraft motions, it does so in the context of modern computational tools and multivariable methods. Robert Stengel devotes particular attention to models and techniques that are appropriate for analysis, simulation, evaluation of flying qualities, and control system design. He establishes bridges to classical analysis and results, and explores new territory that was treated only inferentially in earlier books. This book combines a highly accessible style of presentation with contents that will appeal to graduate students and to professionals already familiar with basic flight dynamics. Dynamic analysis has changed dramatically in recent decades, with the introduction of powerful personal computers and scientific programming languages. Analysis programs have become so pervasive that it can be assumed that all students and practicing engineers working on aircraft flight dynamics have access to them. Therefore, this book presents the principles, derivations, and equations of flight dynamics with frequent reference to MATLAB functions and examples. By using common notation and not assuming a strong background in aeronautics, Flight Dynamics will engage a wide variety of readers. Introductions to aerodynamics, propulsion, structures, flying qualities, flight control, and the atmospheric and gravitational environment accompany the development of the aircraft's dynamic equations.
Author:
Publisher:
Published: 1965
Total Pages: 36
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Published: 1971
Total Pages: 572
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DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1964
Total Pages: 38
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DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1965
Total Pages: 70
ISBN-13:
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