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Damping In Roll Of Models With 45c 60c And 70c Delta Wings Determined At High Subsonic Transonic And Supersonic Speeds With Rocket Powered Models
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Book Synopsis Damping in Roll of Models with 45 Degree, 60 Degree, and 70 Degree Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models by : E. Claude Jr Sanders
Download or read book Damping in Roll of Models with 45 Degree, 60 Degree, and 70 Degree Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models written by E. Claude Jr Sanders and published by . This book was released on 1952 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Sting-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings by : William M. Bland
Download or read book A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Sting-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings written by William M. Bland and published by . This book was released on 1950 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight test technique utilizing rocket-propelled test vehicles with which the damping in roll of sting-mounted wings and wing-fuselage combinations can be obtained over the high subsonic, transonic, and supersonic speed range is described and some results for delta and unswept tapered wings are presented. Initial results compare well with those obtained in supersonic wind-tunnel tests. Results for all of the configurations tested show that damping in roll was maintained throughout the Mach number range investigated and that subsonic damping-in-roll agreed with theoretical values within experimental accuracy. In the lower supersonic region these results differ from the values predicted by linearized flow theory; however, the agreement improved with increasing Mach number. Increased section thickness decreased the damping in roll of the delta wings throughout the Mach number range investigated.
Book Synopsis Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model by : Lewis R. Fisher
Download or read book Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model written by Lewis R. Fisher and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models by : William M. Bland
Download or read book Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models written by William M. Bland and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability Characteristics and Damping in Pitch of Delta Wings by : W. B. McCarter
Download or read book Longitudinal Stability Characteristics and Damping in Pitch of Delta Wings written by W. B. McCarter and published by . This book was released on 1954 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Roll Damping of a Model with Swept-back and Swept-forward Wings by :
Download or read book Subsonic Roll Damping of a Model with Swept-back and Swept-forward Wings written by and published by . This book was released on 1978 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Determination of the Damping in Roll Derivative of a Delta Wing at Supersonic Speed by :
Download or read book Theoretical Determination of the Damping in Roll Derivative of a Delta Wing at Supersonic Speed written by and published by . This book was released on 1960 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Damping in Roll of Rocket-powered Test Vehicles Having Rectangular Wings with NACA 65-006 and Symmetrical Double-wedge Airfoil Sections of Aspect Ratio 4.5 by : Albert E. Dietz
Download or read book The Damping in Roll of Rocket-powered Test Vehicles Having Rectangular Wings with NACA 65-006 and Symmetrical Double-wedge Airfoil Sections of Aspect Ratio 4.5 written by Albert E. Dietz and published by . This book was released on 1950 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight investigation of two rocket-powered model configurations has been made to determine the damping of roll. The models had rectangular wings of 4.5 aspect ratio and were the same except for airfoil section; one configuration had an NACA 65-006 airfoil section and the other had a modified double-wedge airfoil section (6 percent thick). Each model used a rocket motor incorporating a torque nozzle which produced a known torque to roll the model during the accelerated portion of flight. The damping in roll was calculated by balancing the moments acting on the model throughout the accelerating and decelerating portions of flight.
Book Synopsis Transonic Pitch Damping of a Delta Wing Aircraft Determined from Flight Measurements by : R. A. Feik
Download or read book Transonic Pitch Damping of a Delta Wing Aircraft Determined from Flight Measurements written by R. A. Feik and published by . This book was released on 1979 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight investigation aimed mainly at determining the pitch damping of a 60 degree Delta wing aircraft between M = 0.7 and M = 1.2 has been undertaken. Flight tests were conducted by ARDU and the measurements obtained have been successfully analysed at ARL using a modified Newton-Raphson parameter estimation procedure. The results for pitch damping as well as other longitudinal aerodynamic derivatives have been compared with wind tunnel and/or theoretical estimates. Further information has also been gained relating to the necessary conditions for successful extraction of parameters from flight data. The parameter estimation procedure has proved to be an effective analysis method even when only a modest amount of flight data, obtained using a relatively simple instrumentation package, has been available. (Author).
Book Synopsis Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket-propelled Vehicles by : William M. Bland
Download or read book Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket-propelled Vehicles written by William M. Bland and published by . This book was released on 1952 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Data for Zero-lift Damping in Roll of Wing-body Combinations as Determined with Rocket-powered Models Equipped with Roll-torque Nozzles by : David G. Stone
Download or read book A Collection of Data for Zero-lift Damping in Roll of Wing-body Combinations as Determined with Rocket-powered Models Equipped with Roll-torque Nozzles written by David G. Stone and published by . This book was released on 1953 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data by : Charles Harold Wilts
Download or read book Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data written by Charles Harold Wilts and published by . This book was released on 1959 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Ating-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings by : William M. Bland
Download or read book A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Ating-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings written by William M. Bland and published by . This book was released on 1955 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Free-flight Technique for Measuring Damping in Roll by Use of Rocket-powered Models and Some Initial Results for Rectangular Wings by : James L. Edmondson
Download or read book A Free-flight Technique for Measuring Damping in Roll by Use of Rocket-powered Models and Some Initial Results for Rectangular Wings written by James L. Edmondson and published by . This book was released on 1949 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simplified method for obtaining free-flight measurements of damping in roll through use of rocket-powered models has been developed; and initial configurations have been tested through a Mach number range of approximately 0.85 to 1.40, which corresponds to a Reynolds number range of 4,500,000 to 8,000,000. The basic principle of this method is that the model is forced to roll by a non-aerodynamic rolling moment of known magnitude which is produced by a canted-nozzle assembly, and the damping in roll is computed by balancing moments acting on the model.
Book Synopsis Some Data on Elevator Damping and Stiffness Derivatives on a Delta Wing Aircraft Model at Supersonic Speeds by : Kazimierz J. Orlik-Rückemann
Download or read book Some Data on Elevator Damping and Stiffness Derivatives on a Delta Wing Aircraft Model at Supersonic Speeds written by Kazimierz J. Orlik-Rückemann and published by . This book was released on 1959 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
