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Flutter Investigation In The High Subsonic And Transonic Speed Range On Cantilever Delta Wing Plan Forms With Leading Edge Sweepback Of 60 Degrees 53 Degrees 8 Minutes And 45 Degrees
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Book Synopsis Flutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8 Minutes, and 45 Degrees by : William T. Jr Lauten
Download or read book Flutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8 Minutes, and 45 Degrees written by William T. Jr Lauten and published by . This book was released on 1957 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6 by : John R. Unangst
Download or read book Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6 written by John R. Unangst and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Investigation of a Cantilevered, Aspect-ratio-4, 45 Degree Sweptback, Untapered Wing with Three Different Pylon-mounted External Store Configurations by : Charles L. Ruhlin
Download or read book Transonic Flutter Investigation of a Cantilevered, Aspect-ratio-4, 45 Degree Sweptback, Untapered Wing with Three Different Pylon-mounted External Store Configurations written by Charles L. Ruhlin and published by . This book was released on 1957 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brief, exploratory investigation has been made of the transonic flutter characteristics of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external-store configuration. For stores located near the midsemispan and weighing about 0.7 of the semispan wing, the flutter speed was not changed when the store center of gravity was moved from 38 to 12 percent of the chord. The flutter speeds for these two stores were from 14 to 19 percent less than those obtained with the wings alone at subsonic speeds. The rate of rise of flutter speed with Mach number in the low supersonic range was about the same for the wing with stores as for the plain wing.
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 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 Transonic Flutter Investigation of a 64 Degree Delta Wing Constructed with Spars Along Constant-percent Chord Lines and Streamwise Ribs by : George W. Jones
Download or read book Transonic Flutter Investigation of a 64 Degree Delta Wing Constructed with Spars Along Constant-percent Chord Lines and Streamwise Ribs written by George W. Jones and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been made in the Langley transonic blowdown tunnel of the transonic flutter characteristics of a 64 degree delta wing which simulated in a crude manner a construction having spars along constant-percent chord lines and streamwise ribs. The data obtained were compared with previously published data on a 64 degree delta wing with construction which simulated spanwise spars and orthogonal streamwise ribs.
Book Synopsis Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights by : John L. Sewall
Download or read book Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights written by John L. Sewall and published by . This book was released on 1951 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Leading-edge Sweep on Flutter Characteristics of Some Delta-planform Surfaces at a Mach Number of 15.4 by : Robert C. Goetz
Download or read book Effects of Leading-edge Sweep on Flutter Characteristics of Some Delta-planform Surfaces at a Mach Number of 15.4 written by Robert C. Goetz and published by . This book was released on 1964 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Characteristics of an Aspect-ratio-4, 45° Sweptback, Taper-ratio-0.2 Plan Form by : John R. Unangst
Download or read book Transonic Flutter Characteristics of an Aspect-ratio-4, 45° Sweptback, Taper-ratio-0.2 Plan Form written by John R. Unangst and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Study of a 50.5 ̊cropped-delta Wing with Two Rearward-mounted Nacelles by : Maynard C. Sandford
Download or read book Transonic Flutter Study of a 50.5 ̊cropped-delta Wing with Two Rearward-mounted Nacelles written by Maynard C. Sandford and published by . This book was released on 1974 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Gust-tunnel Investigation of a Delta-wing Model with the Leading Edge Swept Back 60 Degrees by : Harold B. Pierce
Download or read book Gust-tunnel Investigation of a Delta-wing Model with the Leading Edge Swept Back 60 Degrees written by Harold B. Pierce and published by . This book was released on 1952 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Flutter Model Tests. Part III. 60 Degree Delta Wings by : John C. Calcerak
Download or read book Transonic Flutter Model Tests. Part III. 60 Degree Delta Wings written by John C. Calcerak and published by . This book was released on 1958 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparisons with Experimental Results by : Homer G. Morgan
Download or read book Procedure for Calculating Flutter at High Supersonic Speed Including Camber Deflections, and Comparisons with Experimental Results written by Homer G. Morgan and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method is used to calculate the flutter speed of some wings which had been previously tested at Mach numbers of 1.3 to 3.0. Comparison of the calculations and experiment is made for flat-plate 60 degrees and 45 degrees delta wings and also for an untapered 45 degree sweptback wing.
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:
