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Aircraft wake turbulence and its detection : proceedings of a symposium on aircraft wake turbulence held in Seattle, Washington, September 1-3, 1970, sponsored jointly by the Flight Sciences Laboratory, Boeing Scientific Research Laboratories and the Air Force Office of Scientific Research. / / edited by John H Olsen, Arnold Goldburg, Milton Rogers
| Aircraft wake turbulence and its detection : proceedings of a symposium on aircraft wake turbulence held in Seattle, Washington, September 1-3, 1970, sponsored jointly by the Flight Sciences Laboratory, Boeing Scientific Research Laboratories and the Air Force Office of Scientific Research. / / edited by John H Olsen, Arnold Goldburg, Milton Rogers |
| Edizione | [1st ed. 1971.] |
| Pubbl/distr/stampa | New York, New York ; ; London : , : Plenum Press, , [1971] |
| Descrizione fisica | 1 online resource (598 p.) |
| Disciplina | 629.13232 |
| Collana | Advisory circular |
| Soggetto topico | Wakes (Aerodynamics) |
| ISBN | 1-4684-8346-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Keynote Address -- Aircraft Wakes: A New Look at a Classical Problem -- Fundamental Problems -- The Velocity of Viscous Vortex Rings -- Studies in the Motion and Decay of Vortices -- Transport of a Vortex Wake in a Stably Stratified Atmosphere -- Experimental Methods -- Split-Film Anemometer Sensors for Three-Dimensional Velocity-Vector Measurement -- Sub-Scale Modeling of Aircraft Trailing Vortices -- The Utility of Doppler Radar in the Study of Aircraft Wing-Tip Vortices -- Application of Laser Doppler Systems to Vortex Measurement and Detection -- Wake Formation and Character -- An Analysis of Flight Measurements in the Wake of a Jet Transport Aircraft -- Vortex Control -- The Effect of a Drooped Wing Tip on Its Trailing Vortex System -- Some Work at the Royal Aircraft Establishment on the Behaviour of Vortex Wakes -- Span Loading and Formation of Wake -- An Experimental Investigation of Trailing Vortices Behind a Wing with a Vortex Dissipator -- Vortex Wake Development and Aircraft Dynamics -- Measurements of Boeing 747, Lockheed C5A and Other Aircraft Vortex Wake Characteristics by Tower Fly-by Technique -- Flight Evaluation of the Wing Vortex Wake Generated by Large Jet Transports -- Stability and Decay -- An Assessment of Dominant Mechanisms in Vortex-Wake Decay -- Theoretical and Experimental Study of the Stability of a Vortex Pair -- Structure of a Line Vortex in an Imposed Strain -- A New Look at the Dynamics of Vortices with Finite Cores -- Decay of an Isolated Vortex -- Decay of a Vortex Pair Behind an Aircraft -- Results of Trailing Vortex Studies in a Towing Tank -- Interactions with Vortex Wakes -- Results of the Boeing Company Wake Turbulence Test Program -- Aircraft Response to Turbulence Including Wakes -- Airloads and Moments on an Aircraft Flying Over a Pair of Inclined Trailing Vortices -- Aircraft Wake Turbulence Controllability Experiment -- Fog Formation and Dispersal by Trailing Vortices -- An Estimate of the Power Required to Eliminate Trailing Vortices by Suction -- Panel Discussion -- Conclusions -- Author Index. |
| Record Nr. | UNINA-9910698683603321 |
| New York, New York ; ; London : , : Plenum Press, , [1971] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Stress-Corrosion Cracking of Titanium
| Stress-Corrosion Cracking of Titanium |
| Pubbl/distr/stampa | [Place of publication not identified], : American Society for Testing & Materials, 1966 |
| Descrizione fisica | 1 online resource (259 pages) : illustrations |
| Disciplina | 624.1776 |
| Collana | ASTM special technical publication |
| Soggetto topico | Titanium alloys - Fatigue |
| ISBN | 0-8031-6800-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910164270503321 |
| [Place of publication not identified], : American Society for Testing & Materials, 1966 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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