Studies of Optimum Body Shapes at Hypersonic Speeds

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Studies of Optimum Body Shapes at Hypersonic Speeds by : Louis S. Stivers

Download or read book Studies of Optimum Body Shapes at Hypersonic Speeds written by Louis S. Stivers and published by . This book was released on 1967 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Studies Relating to the Attainment of High Lift-drag Ratios at Hypersonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Studies Relating to the Attainment of High Lift-drag Ratios at Hypersonic Speeds by :

Download or read book Studies Relating to the Attainment of High Lift-drag Ratios at Hypersonic Speeds written by and published by . This book was released on 1965 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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Publisher :
ISBN 13 :
Total Pages : 598 pages
Book Rating : 4.:/5 (35 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1977 with total page 598 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Theory of Optimum Aerodynamic Shapes

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ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Theory of Optimum Aerodynamic Shapes by : Angelo Miele

Download or read book Theory of Optimum Aerodynamic Shapes written by Angelo Miele and published by . This book was released on 1965 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Aerodynamic Characteristics of Minimum-wave-drag Bodies Having Variations in Cross-sectional Shape

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Hypersonic Aerodynamic Characteristics of Minimum-wave-drag Bodies Having Variations in Cross-sectional Shape by : Bernard Spencer

Download or read book Hypersonic Aerodynamic Characteristics of Minimum-wave-drag Bodies Having Variations in Cross-sectional Shape written by Bernard Spencer and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Aerodynamic Characteristics of Hypersonic Low-wave-drag Elliptical-body-tail Combinations as Affected by Changes in Stabilizer Configuration

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Transonic Aerodynamic Characteristics of Hypersonic Low-wave-drag Elliptical-body-tail Combinations as Affected by Changes in Stabilizer Configuration by : Charles H. Fox

Download or read book Transonic Aerodynamic Characteristics of Hypersonic Low-wave-drag Elliptical-body-tail Combinations as Affected by Changes in Stabilizer Configuration written by Charles H. Fox and published by . This book was released on 1969 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 by : Walter P. Nelms

Download or read book Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 written by Walter P. Nelms and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The configuration had a delta planform with an elliptic cone forebody and an afterbody of elliptic cross section. Detailed effects of varying angle of attack (-2 to 15 deg), angle of sideslip (-2 to 8 deg), Mach number, and configuration buildup were considered. In addition, the effectiveness of horizontal tail, vertical tail, and canard stabilizing and control surfaces was investigated. The results indicate that all configurations were longitudinally stable near maximum lift drag ratio. The configurations with vertical tails were directionally stable at all angles of attack. Trim penalties were small at hypersonic speeds for a center of gravity location representative of the airplane, but because of the large rearward travel of the aerodynamic center, trim penalties were severe at transonic Mach numbers.

NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 448 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1968 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Flow Research

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Publisher : Elsevier
ISBN 13 : 0323142621
Total Pages : 769 pages
Book Rating : 4.3/5 (231 download)

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Book Synopsis Hypersonic Flow Research by : F.R. Riddell

Download or read book Hypersonic Flow Research written by F.R. Riddell and published by Elsevier. This book was released on 2012-12-02 with total page 769 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.

Effect of Geometric Modifications on the Maximum Lift-drag Ratios of Slender Wing-body Configurations at Hypersonic Speeds

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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of Geometric Modifications on the Maximum Lift-drag Ratios of Slender Wing-body Configurations at Hypersonic Speeds by : William J. Small

Download or read book Effect of Geometric Modifications on the Maximum Lift-drag Ratios of Slender Wing-body Configurations at Hypersonic Speeds written by William J. Small and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Optimum Shape of a Blunt Forebody in Hypersonic Flow

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Optimum Shape of a Blunt Forebody in Hypersonic Flow by : Institute for Computer Applications in Science and Engineering

Download or read book Optimum Shape of a Blunt Forebody in Hypersonic Flow written by Institute for Computer Applications in Science and Engineering and published by . This book was released on 1989 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction to Hypersonic Flow

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Publisher : Academic Press
ISBN 13 : 1483271684
Total Pages : 277 pages
Book Rating : 4.4/5 (832 download)

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Book Synopsis Introduction to Hypersonic Flow by : G. G. Chernyi

Download or read book Introduction to Hypersonic Flow written by G. G. Chernyi and published by Academic Press. This book was released on 2013-10-22 with total page 277 pages. Available in PDF, EPUB and Kindle. Book excerpt: Introduction to Hypersonic Flow has been made available to the English speaking reader because of its usefulness for those individuals desirous of obtaining an introduction to the subject. Written by an internationally acknowledged expert in the field of hypersonic flow, the book makes available heretofore unpublished Soviet work, as well as published work little known outside the Soviet Union. The author has however made every effort to include, where appropriate. Western references for the work he discusses. Starting with a general introductory chapter on hypersonic aerodynamics and aerodynamic problems, the remainder of the book concentrates on the inviscid, perfect fluid aspects of hypersonic flow, with emphasis on the fundamental concepts and rational methods of calculation. The book is directed to students of aerodynamics and gas dynamics, as well as to scientists and engineers interested in problems of hypersonic flight. The level of approach is such that it should prove particularly useful as an undergraduate and introductory graduate text.

Hypersonic Aerodynamic Performance of Minimum-wave-drag Bodies

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Aerodynamic Performance of Minimum-wave-drag Bodies by :

Download or read book Hypersonic Aerodynamic Performance of Minimum-wave-drag Bodies written by and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies

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ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies by : Louis S. Stiver

Download or read book Calculated Pressure Distributions and Components of Total-drag Coefficients for 18 Constant-volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, with Experimental Aerodynamic Characteristics for Three of the Bodies written by Louis S. Stiver and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Journal of the Astronautical Sciences

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ISBN 13 :
Total Pages : 560 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Journal of the Astronautical Sciences by :

Download or read book The Journal of the Astronautical Sciences written by and published by . This book was released on 1968 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds by : H. Reese Ivey

Download or read book A Method for Determining the Aerodynamic Characteristics of Two- and Three-dimensional Shapes at Hypersonic Speeds written by H. Reese Ivey and published by . This book was released on 1948 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed for calculating the pressures on aerodynamic shapes at very high supersonic speeds in dense air with the ratio of specific heats equal to 1. The method is applicable to any body of revolution at zero angle of attack and to any two-dimensional profile. The results of the present paper are compared with previous work of Von Karman and Epstein on this problem and the difference explained.