Review of Basic Principles of V/STOL Aerodynamics
Author | : Richard E. Kuhn |
Publisher | : |
Total Pages | : 22 |
Release | : 1961 |
Genre | : |
ISBN | : |
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Author | : Richard E. Kuhn |
Publisher | : |
Total Pages | : 22 |
Release | : 1961 |
Genre | : |
ISBN | : |
Author | : Richard E. Kuhn |
Publisher | : |
Total Pages | : 17 |
Release | : 1961 |
Genre | : |
ISBN | : |
Author | : Barnes Warnock McCormick |
Publisher | : Courier Corporation |
Total Pages | : 356 |
Release | : 1999-01-01 |
Genre | : Technology & Engineering |
ISBN | : 9780486404608 |
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author | : |
Publisher | : |
Total Pages | : 430 |
Release | : 1963 |
Genre | : |
ISBN | : |
Author | : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development |
Publisher | : |
Total Pages | : 522 |
Release | : 1968 |
Genre | : Aerodynamic load |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 355 |
Release | : 1974 |
Genre | : |
ISBN | : |
After 20 years of research, the western world has one operational V/STOL aircraft and that is a military aircraft. An examination of the technical reasons for this failure to convert research results to hardware indicates that the penalties for V/STOL capability are still too large for most applications. This cost may be reduced by improved efficiency of the propulsive lift components and use of the newly emerging augmentor technology. Payload-weight ratios of V/STOL aircraft are 10 to 20%; thus the productivity of the aircraft is very sensitive to small deficiencies or improvements in the various component efficiencies. The state of the art of some of these critical technological areas is reviewed. In particular, STOL augmentors, ground effects, and prediction methods are reviewed briefly. For VTOL, induced aerodynamics, vectoring devices, and modeling problems are reviewed. Research in these areas may significantly reduce the cost of V/STOL performance.
Author | : |
Publisher | : |
Total Pages | : 380 |
Release | : 1960 |
Genre | : Short take-off and landing aircraft |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 252 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Author | : James A. Franklin |
Publisher | : AIAA |
Total Pages | : 240 |
Release | : 2002 |
Genre | : Airplanes |
ISBN | : 9781600860478 |
Annotation This text presents the principles of dynamics and control for vertical, short take-off landing (V/STOL) aircraft. It is the first book of its kind. It is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static, dynamic stability, and control. The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1960-07 |
Genre | : |
ISBN | : |