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Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (141 download)
Download or read book Determination of the Lateral Stability Derivative of a Delta Wing Oscillating in Supersonic Flow written by and published by . This book was released on 1960 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Dean R. Chapman
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ISBN 13 :
Total Pages : 206 pages
Book Rating : 4.3/5 (243 download)
Download or read book Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw written by Dean R. Chapman and published by . This book was released on 1958 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Albert E. Brown
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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)
Download or read book Analysis of the Dynamic Lateral Stability of a Delta-wing Airplane with Frequency-dependent Stability Derivatives written by Albert E. Brown and published by . This book was released on 1959 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lewis R. Fisher
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.3/5 (91 download)
Download or read book Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60© Delta-wing Airplane Model written by Lewis R. Fisher and published by . This book was released on 1958 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lewis R. Fisher
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (317 download)
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:
Author : Charles P. Llewellyn
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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effect of Reynolds Number on the Lateral-stability Derivatives at Low Speed of Swept-back and Delta-wing-fuselage Combinations Oscillating in Yaw written by Charles P. Llewellyn and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to determine the effect of Reynolds number on the lateral-stability derivatives at low speed of sweptback- and delta-wing-fuselage combinations. Results were obtained from the models oscillating in yaw over an angle-of-attack ...
Author : John A. Moore
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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)
Download or read book Experimental Determination of Damping in Pitch of Swept and Delta Wings at Supersonic Mach Numbers written by John A. Moore and published by . This book was released on 1957 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The damping-in-pitch derivative was determined experimentally at Mach numbers of 2.96 and 3.92 for two delta wings having aspect ratios of 2 and 3 and for one sweptback tapered wing having an aspect ratio of 3 by using a free-oscillation technique. The tests were made at Reynolds numbers based on mean aerodynamic chord from 4,000,000 to 12,000,000 for an angle-of-attack range of zero to 10 degrees. The reduced-frequency parameter ranged from 0.006 to 0.022.
Author : Lewis R. Fisher
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (722 download)
Download or read book Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw written by Lewis R. Fisher and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Effects of amplitude of oscillation on the stability derivatives for the delta wing were evident for certain high angles of attack and for the lowest frequencies of oscillation. As the frequency became high, the amplitude effects tended to disappear.
Author : John W. Paulson
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Low-speed Measurements of Oscillatory Lateral Stability Derivatives of a Model of 60° Delta-wing Bomber written by John W. Paulson and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jacob H. Lichtenstein
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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)
Download or read book Low-speed Investigation of the Effects of Frequency and Amplitude of Oscillation in Sideslip on the Lateral Stability Derivatives of a 60 Degree Delta Wing, a 40 Degree Sweptback Wing and an Unswept Wing written by Jacob H. Lichtenstein and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Herman S. Fletcher
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ISBN 13 :
Total Pages : 45 pages
Book Rating : 4.:/5 (692 download)
Download or read book Low-speed Experimental Determination of the Effects of Leading-edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60 Degrees of Leading-edge Sweep written by Herman S. Fletcher and published by . This book was released on 1958 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley stability tunnel to determine the effects of leading-edge radius and profile thickness on the oscillatory lateral stability derivatives for a series of delta wings with 60 degrees of leading-edge sweep. The wings were oscillated in yaw about their vertical axes.
Author : Sidney M. Harmon
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)
Download or read book Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow written by Sidney M. Harmon and published by . This book was released on 1949 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.
Author : Clarence L. Gillis
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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)
Download or read book Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds written by Clarence L. Gillis and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test and analysis method is presented for determining airplane lateral stability characteristics, including aerodynamic derivatives, from flight tests of scale models. The method of analysis utilizes the rotating time-vector concept and also a quasi-static approach. Data are presented at transonic speeds for three swept-wing rocket-propelled models differing only in vertical position and dihedral of the wing. The method proved to be adequate for delineating the major effects of the geometric variations on the aerodynamic lateral stability derivatives. The effects of Reynolds number on the linearity of the static stability data for an unswept wing configuration are illustrated.
Author : Charles P. Llewellyn
Publisher :
ISBN 13 :
Total Pages : 45 pages
Book Rating : 4.:/5 (249 download)
Download or read book Effect of Reynolds Number on the Lateral-stability Derivatives at Low Speed of Sweptback- and Delta-wing-fuselage Combinations Oscillating in Yaw written by Charles P. Llewellyn and published by . This book was released on 1960 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lewis R. Fisher
Publisher :
ISBN 13 :
Total Pages : 67 pages
Book Rating : 4.:/5 (722 download)
Download or read book Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw written by Lewis R. Fisher and published by . This book was released on 1956 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: Effects of amplitude of oscillation on the stability derivatives for the delta wing were evident for certain high angles of attack and for the lowest frequencies of oscillation. As the frequency became high, the amplitude effects tended to disappear.
Author : Herbert S. Ribner
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)
Download or read book Stability Derivatives of Triangular Wings at Supersonic Speeds written by Herbert S. Ribner and published by . This book was released on 1948 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds, given in NACA TN No. l423, is extended to apply to triangular wings having large vertex angles and traveling at supersonic speeds. The lift, rolling moment due to siderlip, and damping in roll and pitch for this more general case have been treated elsewhere on the basis of the theory of small disturbances.
Author : Lewis R. Fisher
Publisher :
ISBN 13 :
Total Pages : 27 pages
Book Rating : 4.:/5 (248 download)
Download or read book Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw written by Lewis R. Fisher and published by . This book was released on 1958 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
