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Author : E. A. Brong
Publisher :
ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.E/5 ( download)
Download or read book The Unsteady Flow Field about a Right Circular Cone in Unsteady Flight written by E. A. Brong and published by . This book was released on 1967 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : E. A. Brong
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (11 download)
Download or read book The Unsteady Flow Field about a Right Circular Cone in Unsteady Flight written by E. A. Brong and published by . This book was released on 1967 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: The inviscid flow field about a right circular cone in unsteady planar flight is analyzed by a perturbation technique which is an extension of Stone's treatment of the cone at small yaw. A solution is found in the form of infinite series in the time rates of change of the pitch rate and angle of attack. The linear stability derivatives as well as 'higher order' stability derivatives are presented for a wide range of cone angles and Mach numbers. The stability derivatives as obtained from this solution are compared to results obtained from second order potential theory, Newtonian impact theory, and an unsteady flow theory due to Zartarian, Hsu, and Ashley. Both the potential theory and the impact theory predict that the stability derivative (angle of attack) approaches a value which is on the order of 10 percent to 20 percent of the stability derivative (pitch rate). Numerical results obtained from the present theory are also compared to ground-test data. The agreement is found to be generally good, although the data in some instances indicate a pronounced Reynolds number effect.
Author :
Publisher :
ISBN 13 :
Total Pages : 1470 pages
Book Rating : 4.:/5 (319 download)
Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1967-05 with total page 1470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 910 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 910 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)
Download or read book Unsteady Newton-Busemann Flow Theory. Part 2: Bodies of Revolution written by and published by . This book was released on 1981 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Defense Documentation Center (U.S.)
Publisher :
ISBN 13 :
Total Pages : 784 pages
Book Rating : 4.:/5 (1 download)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 1018 pages
Book Rating : 4.:/5 (318 download)
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1967 with total page 1018 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 522 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Aeronautical Journal written by and published by . This book was released on 1995 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : L. A. Marshall
Publisher :
ISBN 13 :
Total Pages : 98 pages
Book Rating : 4.3/5 (91 download)
Download or read book Hypersonic Dynamic Stability written by L. A. Marshall and published by . This book was released on 1967 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents a summary of the important results obtained on a combined analytical and experimental program for investigation of the hypersonic dynamic stability of re-entry vehicles. An unsteady flow field solution is described which predicts the static and dynamic stability characteristics for vehicles which are executing small amplitude oscillations about zero angle of attack. Solutions were obtained for sharp and blunted, axisymmetric and two-dimensional shapes in real gas equilibrium flow. The experimental program was conducted in AEDC tunnel 'C' at Mach 10 and in the Ling-Temco-Vought Hot Shot tunnel at Mach 14 and 20 to obtain dynamic stability characteristics of a 10 degree cone. Data are presented to show the effect of bluntness ratio, reduced frequency, center of gravity location, Reynolds number and Mach number. Comparisons are made with various theoretical results and limited correlations are shown which establish significant trends.
Author : Kazimierz J. Orlick-Rückemann
Publisher :
ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.E/5 ( download)
Download or read book Dynamic Viscous Interaction in Hypersonic Flow written by Kazimierz J. Orlick-Rückemann and published by . This book was released on 1970 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 408 pages
Book Rating : 4.:/5 (319 download)
Download or read book Aeronautical Report written by and published by . This book was released on 1970 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.F/5 ( download)
Download or read book Hypersonic Aerothermodynamics written by and published by . This book was released on 1984 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Volume of Technical Papers Presented Baltimore, Maryland, March 28-30, 1966 written by and published by . This book was released on 1966 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 1014 pages
Book Rating : 4.:/5 (334 download)
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1966-11 with total page 1014 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. H. Urban
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)
Download or read book Dynamic Stability Characteristics of a 10-deg Cone at Mach Number 20 written by R. H. Urban and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Martin C. Jischke
Publisher :
ISBN 13 :
Total Pages : 414 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aerodynamics of Supersonic Lifting Bodies written by Martin C. Jischke and published by . This book was released on 1981 with total page 414 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a combined theoretical and experimental program of research in the aerodynamics of supersonic lifting bodies. Analytical perturbation techniques are used to study the supersonic flow past slightly elliptical cones, cones whose cross-sections deviate slightly but arbitrarily from that of a right circular cone, cones of small longitudinal curvature, and right circular cones undergoing small harmonic pitching and/or plunging motions. These studies all involve perturbations of the well-known solution for supersonic flow past a right circular cone. Closed-form analytical results are achieved through the use of an approximation that accurately predicts results over the entire range of the hypersonic similarity parameter. These results give hypersonic limiting solutions that agree well with other independent analyses and, at the same time, agree exactly with linearized theory in the linear theory limit. Comparisons with experiment, where possible, also show good agreement.
Author :
Publisher :
ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.:/5 (318 download)
Download or read book The Aeronautical Quarterly written by and published by . This book was released on 1979 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
