Comparison of Calculated and Measured Model Rotor Loading and Wake Geometry

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Comparison of Calculated and Measured Model Rotor Loading and Wake Geometry by : Wayne Johnson

Download or read book Comparison of Calculated and Measured Model Rotor Loading and Wake Geometry written by Wayne Johnson and published by . This book was released on 1980 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Calculated and Measured Helicopter Rotor Lateral Flapping Angles

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Comparison of Calculated and Measured Helicopter Rotor Lateral Flapping Angles by :

Download or read book Comparison of Calculated and Measured Helicopter Rotor Lateral Flapping Angles written by and published by . This book was released on 1980 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wake Geometry Measurements and Analytical Calculations on a Small-Scale Rotor Model

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Publisher : Independently Published
ISBN 13 : 9781730900822
Total Pages : 70 pages
Book Rating : 4.9/5 (8 download)

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Book Synopsis Wake Geometry Measurements and Analytical Calculations on a Small-Scale Rotor Model by : National Aeronautics and Space Adm Nasa

Download or read book Wake Geometry Measurements and Analytical Calculations on a Small-Scale Rotor Model written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-05 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the Langley 14- by 22-Foot Subsonic Tunnel to quantify the rotor wake behind a scale model helicopter rotor in forward level flight at one thrust level. The rotor system in this test consisted of a four-bladed fully articulated hub with blades of rectangular planform and an NACA 0012 airfoil section. A laser light sheet, seeded with propylene glycol smoke, was used to visualize the vortex geometry in the flow in planes parallel and perpendicular to the free-stream flow. Quantitative measurements of wake geometric proper- ties, such as vortex location, vertical skew angle, and vortex particle void radius, were obtained as well as convective velocities for blade tip vortices. Comparisons were made between experimental data and four computational method predictions of experimental tip vortex locations, vortex vertical skew angles, and wake geometries. The results of these comparisons highlight difficulties of accurate wake geometry predictions. Ghee, Terence A. and Berry, John D. and Zori, Laith A. J. and Elliott, Joe W. Unspecified Center...

Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel

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ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel by :

Download or read book Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel written by and published by . This book was released on 2001 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comparisons of measured and calculated aerodynamic behavior of a tiltrotor model are presented. The test of the Tilt Rotor Aeroacoustic Model (TRAM) with a single, 0.25-scale V-22 rotor in the German-Dutch Wind Tunnel (DNW) provides an extensive set of aeroacoustic, performance, and structural loads data. The calculations were performed using the rotorcraft comprehensive analysis CAMRAD II. Presented are comparisons of measured and calculated performance for hover and helicopter mode operation, and airloads for helicopter mode. Calculated induced power, profile power, and wake geometry provide additional information about the aerodynamic behavior. An aerodynamic and wake model and calculation procedure that reflects the unique geometry and phenomena of tiltrotors has been developed. There are major differences between this model and the corresponding aerodynamic and wake model that has been established for helicopter rotors. In general, good correlation between measured and calculated performance and airloads behavior has been shown. Two aspects of the analysis that clearly need improvement are the stall delay model and the trailed vortex formation model.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 556 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1993 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Development and Application of a Method for Predicting Rotor Free Wake Positions and Resulting Rotor Blade Air Loads

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Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Development and Application of a Method for Predicting Rotor Free Wake Positions and Resulting Rotor Blade Air Loads by : S. Gene Sadler

Download or read book Development and Application of a Method for Predicting Rotor Free Wake Positions and Resulting Rotor Blade Air Loads written by S. Gene Sadler and published by . This book was released on 1971 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rotor wake geometries are predicted by a process similar to the startup of a rotor in a free stream. An array of discrete trailing and shed vortices is generated with vortex strengths corresponding to stepwise radial and azimuthal blade circulations. The array of shed and trailing vortices is limited to an arbitrary number of azimuthal steps behind each blade. The remainder of the wake model of each blade is an arbitrary number of trailing vortices. Vortex element end points were allowed to be transported by the resultant velocity of the free stream and vortex-induced velocities. Wake geometry, wake flow, and wake-induced velocity influence coefficients are generated by this program for use in the blade loads portion of the calculations. Blade loads computations include the effects of nonuniform inflow due to a free wake, nonlinear airfoil characteristics, and response of flexible blades to the applied loads. Computed wake flows and blade loads are compared with experimentally measured data. Predicted blade loads, response and shears and moments are obtained for a model rotor system having two independent rotors. The effects of advance ratio, vertical separation of rotors, different blade radius ratios, and different azimuthal spacing of the blades of one rotor with respect to the other are investigated.

A Full Potential Flow Analysis with Realistic Wake Influence for Helicopter Rotor Airload Prediction

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Publisher :
ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis A Full Potential Flow Analysis with Realistic Wake Influence for Helicopter Rotor Airload Prediction by : T. Alan Egolf

Download or read book A Full Potential Flow Analysis with Realistic Wake Influence for Helicopter Rotor Airload Prediction written by T. Alan Egolf and published by . This book was released on 1987 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Calculated and Measured Pressures on Straight and Swept-tip Model Rotor Blades

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Comparison of Calculated and Measured Pressures on Straight and Swept-tip Model Rotor Blades by :

Download or read book Comparison of Calculated and Measured Pressures on Straight and Swept-tip Model Rotor Blades written by and published by . This book was released on 1983 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Finite Difference Modeling of Rotor Flows Including Wake Effects

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Finite Difference Modeling of Rotor Flows Including Wake Effects by :

Download or read book Finite Difference Modeling of Rotor Flows Including Wake Effects written by and published by . This book was released on 1982 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper gives a brief consideration of rotary wing finite difference methods. The main concern is the specification of boundary conditions to properly account for the effect of the wake on the blade. Examples are given of an approach where wake effects are introduced by specifying an equivalent angle of attack. An alternate approach is also given where discrete vortices are introduced into the finite difference grid. The resulting computations of hovering and high advance-ratio cases compare well with experiment. Some consideration is also given to the modeling of low-to-moderate advance-ratio flows. (Author).

A Lifting Surface Performance Analysis with Circulation Coupled Wake for Advanced Configuration Hovering Rotors

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Publisher :
ISBN 13 :
Total Pages : 400 pages
Book Rating : 4.:/5 (454 download)

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Book Synopsis A Lifting Surface Performance Analysis with Circulation Coupled Wake for Advanced Configuration Hovering Rotors by : James David Kocurek

Download or read book A Lifting Surface Performance Analysis with Circulation Coupled Wake for Advanced Configuration Hovering Rotors written by James David Kocurek and published by . This book was released on 1978 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hovering Measurements for Twin-rotor Configurations with and Without Overlap

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Hovering Measurements for Twin-rotor Configurations with and Without Overlap by : George E. Sweet

Download or read book Hovering Measurements for Twin-rotor Configurations with and Without Overlap written by George E. Sweet and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Free Wake Techniques for Rotor Aerodynamic Analysis. Volume 3: Vortex Filament Models

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Free Wake Techniques for Rotor Aerodynamic Analysis. Volume 3: Vortex Filament Models by :

Download or read book Free Wake Techniques for Rotor Aerodynamic Analysis. Volume 3: Vortex Filament Models written by and published by . This book was released on 1982 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Assessment of Aerodynamic and Dynamic Models in a Comprehensive Analysis

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Assessment of Aerodynamic and Dynamic Models in a Comprehensive Analysis by :

Download or read book Assessment of Aerodynamic and Dynamic Models in a Comprehensive Analysis written by and published by . This book was released on 1985 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 340 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Rotor Induced-inflow-ratio Measurements and CAMRAD Calculations

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Rotor Induced-inflow-ratio Measurements and CAMRAD Calculations by : Danny R. Hoad

Download or read book Rotor Induced-inflow-ratio Measurements and CAMRAD Calculations written by Danny R. Hoad and published by . This book was released on 1990 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1388 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1971 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications, Cumulative Index

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ISBN 13 :
Total Pages : 1466 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents

Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt: