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Flutter Of A 60c Delta Wing Naca 65a003 Airfoil Encountered At Supersonic Speeds During The Flight Test Of A Rocket Propelled Model
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Book Synopsis Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model by : Joseph H. Judd
Download or read book Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model written by Joseph H. Judd and published by . This book was released on 1952 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model by : William T. Jr Lauten
Download or read book Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model written by William T. Jr Lauten and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model by : William T. Lauten
Download or read book Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model written by William T. Lauten and published by . This book was released on 1951 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis of the flight time history of a rocket-propelled model of a 60 degrees delta-wing airplane configuration, fired for the purpose of obtaining zero-lift drag data, indicated wing flutter and subsequent failure at low-supersonic Mach numbers. This flutter occurred during the unpowered decelerating portion of the flight. The behavior of the model during flight is discussed and the mass and stiffness characteristics of a duplicate wing are presented.
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 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section by : William C. Sleeman
Download or read book Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Book Synopsis Flight Test and Analysis of the Rolling Motions of a 79 ̊clipped Delta Configuration with Wing-tip Fins at Supersonic Speeds by : James L. Raper
Download or read book Flight Test and Analysis of the Rolling Motions of a 79 ̊clipped Delta Configuration with Wing-tip Fins at Supersonic Speeds written by James L. Raper and published by . This book was released on 1963 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Swept and Delta Wing Sense written by and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Leading- and Trailing-edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds by : Gloria Hernandez
Download or read book Effect of Leading- and Trailing-edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds written by Gloria Hernandez and published by . This book was released on 1994 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 by : Robert S. Osborne
Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Influence of Airfoil Geometry on Delta Wing Leading-edge Vortices and Vortex-induced Aerodynamics at Supersonic Speeds by : Richard M. Wood
Download or read book Influence of Airfoil Geometry on Delta Wing Leading-edge Vortices and Vortex-induced Aerodynamics at Supersonic Speeds written by Richard M. Wood and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Professional Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing by : Earl R. Keener
Download or read book Professional Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing written by Earl R. Keener and published by . This book was released on 1959 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study and Analysis of Loading and Pressure Distributions on Delta Wings Due to Thickness and to Angle of Attack at Supersonic Speeds by : William B. Boatright
Download or read book Experimental Study and Analysis of Loading and Pressure Distributions on Delta Wings Due to Thickness and to Angle of Attack at Supersonic Speeds written by William B. Boatright and published by . This book was released on 1956 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic loading on delta wings at supersonic speed was studied principally to determine the coupling and nonlinear interference effects between the pressures due to angle of attack and due to thickness. Pressure distributions on four delta wings having leading-edge sweep angles of 53, 60, and 66.6 degrees were measured at Mach numbers of 1.62, 1.93, and 2.41. Three wings had NACA 65A003 sections. The other wing had a flat upper surface and a leading-edge sweep angle of 53 degrees. At Mach numbers of 1.94 and 2.41, some of the results for this wing simulate a wing of zero thickness; the pressure distributions are compared with the pressure distributions of an NACA 65A003 section wing of the same plan form. For this comparison the pressure distributions at zero angle of attack deducted. Appreciable nonlinear interference effects are shown to exist such that the pressure distributions caused by angle of attack are not additive at test angles of attack greater than 5 degrees. These effects are shown to exist for all the NACA 65A003 section wings at all test Mach numbers, and in each case the experimental results are compared with theory.
Book Synopsis Description and Analysis of a Rocket-vehicle Experiment on Flutter Involving Wing Deformation and Body Motions by : H. J. Cunningham
Download or read book Description and Analysis of a Rocket-vehicle Experiment on Flutter Involving Wing Deformation and Body Motions written by H. J. Cunningham and published by . This book was released on 1950 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight tests and a mathematical analysis were made to demonstrate and confirm a type of subsonic flutter involving rigid-body motions and wing deformations. For the configuration considered the period of the oscillation was approximately 100 chords per cycle which is well within the range of period found in dynamic-stability work on rigid aircraft with free controls. A mathematical analysis based on two-dimensional incompressible flow provided a conservative prediction of the airspeed at which the low-frequency flutter occurred. It was found that wing bending stiffness is the important parameter for preventing such flutter.
Book Synopsis A Transonic Wind-tunnel Investigation of the Longitudinal Force and Moment Characteristics of Two Delta Wings and One Clipped-tip Delta Wing of 4 Percent Thickness on a Slender Body by : William E. Palmer
Download or read book A Transonic Wind-tunnel Investigation of the Longitudinal Force and Moment Characteristics of Two Delta Wings and One Clipped-tip Delta Wing of 4 Percent Thickness on a Slender Body written by William E. Palmer and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flutter Experiences with Thin Pointed-tip Wings During Flight Tests of Rocket-propelled Models at Mach Numbers from 0.8 to 1.95 by : Harvey A. Wallskog
Download or read book Flutter Experiences with Thin Pointed-tip Wings During Flight Tests of Rocket-propelled Models at Mach Numbers from 0.8 to 1.95 written by Harvey A. Wallskog and published by . This book was released on 1955 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
