Aerodynamic characteristics of ogive oversize-head cylinders stabilized by tail-mounted, multiple fins or ring wings at supersonic mach numbers

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (15 download)

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Book Synopsis Aerodynamic characteristics of ogive oversize-head cylinders stabilized by tail-mounted, multiple fins or ring wings at supersonic mach numbers by : Klaus O. Opalka

Download or read book Aerodynamic characteristics of ogive oversize-head cylinders stabilized by tail-mounted, multiple fins or ring wings at supersonic mach numbers written by Klaus O. Opalka and published by . This book was released on 1973 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test data are reported for two ring-wing and two multiple-fin stabilizers mounted on the tail of a cylinder combined with ogive oversize heads of 1.38 caliber diameter and varying lengths. Wind tunnel tests were run at five (5) Mach numbers from 1.75 to 3.5 and the resulting aerodynamic coefficients are plotted versus angle of attack and Mach number. The results are discussed regarding their effects on the longitudinal stability for the various configurations. (Author).

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 960 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Government Reports Announcements

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ISBN 13 :
Total Pages : 670 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Government Reports Announcements by :

Download or read book Government Reports Announcements written by and published by . This book was released on 1973 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1296 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Government Reports Announcements & Index by :

Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1973 with total page 1296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Index

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ISBN 13 :
Total Pages : 1068 pages
Book Rating : 4.3/5 (129 download)

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Book Synopsis Government Reports Index by :

Download or read book Government Reports Index written by and published by . This book was released on 1973 with total page 1068 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Surface Flow Angles on an Ogive Cylinder at Angle of Attack in Supersonic Flow

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Surface Flow Angles on an Ogive Cylinder at Angle of Attack in Supersonic Flow by : Harold R. Vaughn

Download or read book Surface Flow Angles on an Ogive Cylinder at Angle of Attack in Supersonic Flow written by Harold R. Vaughn and published by . This book was released on 1971 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach numbers. The results are compared with potential theory which is shown to be inadequate unitl modified.

Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds by : Charles H. McLellan

Download or read book Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds written by Charles H. McLellan and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.

Effect of Several Tail Configurations on the Stability Characteristics of a Midwing Supersonic-bomber Model at Mach Numbers of 1.60, 1.90, 2.20, and 2.50

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of Several Tail Configurations on the Stability Characteristics of a Midwing Supersonic-bomber Model at Mach Numbers of 1.60, 1.90, 2.20, and 2.50 by :

Download or read book Effect of Several Tail Configurations on the Stability Characteristics of a Midwing Supersonic-bomber Model at Mach Numbers of 1.60, 1.90, 2.20, and 2.50 written by and published by . This book was released on 1960 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Aerodynamic Characteristics at High Subsonic Speeds of Two Supersonic- Cruise Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips

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ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Investigation of Aerodynamic Characteristics at High Subsonic Speeds of Two Supersonic- Cruise Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips by :

Download or read book Investigation of Aerodynamic Characteristics at High Subsonic Speeds of Two Supersonic- Cruise Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips written by and published by . This book was released on 1960 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration

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ISBN 13 :
Total Pages : 842 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration by : Frank S. Malvestuto

Download or read book Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration written by Frank S. Malvestuto and published by . This book was released on 1951 with total page 842 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.

Design for Control of Projectile Flight Characteristics

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ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Design for Control of Projectile Flight Characteristics by : United States. Army Materiel Command

Download or read book Design for Control of Projectile Flight Characteristics written by United States. Army Materiel Command and published by . This book was released on 1966 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Supersonic Aerodynamics

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ISBN 13 :
Total Pages : 516 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md and published by . This book was released on 1961 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Encyclopedia of Aerodynamics

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Publisher : Andrews UK Limited
ISBN 13 : 1785383248
Total Pages : 677 pages
Book Rating : 4.7/5 (853 download)

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Book Synopsis The Encyclopedia of Aerodynamics by : Frank Hitchens

Download or read book The Encyclopedia of Aerodynamics written by Frank Hitchens and published by Andrews UK Limited. This book was released on 2015-11-25 with total page 677 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Encyclopedia of Aerodynamics was written for pilots at all levels from private pilot to airline pilot, military pilots and students of aerodynamics as a complete reference manual to aerodynamic terminology. General aerodynamic text books for pilots are relatively limited in their scope while aerodynamic text books for engineering students involve complex calculus. The references in this book, The Encyclopedia of Aerodynamics, are clearly described and only basic algebra is used in a few references but is completely devoid of any calculus - an advantage to many readers. Over 1400 references are included with alternative terms used where appropriate and cross-referenced throughout. The text is illustrated with 178 photographs and 96 diagrams. The Encyclopedia of Aerodynamics is an ideal aerodynamic reference manual for any pilot's bookshelf.

Hypersonic and High Temperature Gas Dynamics

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Publisher : AIAA
ISBN 13 : 9781563474590
Total Pages : 710 pages
Book Rating : 4.4/5 (745 download)

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Book Synopsis Hypersonic and High Temperature Gas Dynamics by : John David Anderson

Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Tactical Missile Aerodynamics

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ISBN 13 : 9781563470158
Total Pages : 731 pages
Book Rating : 4.4/5 (71 download)

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Book Synopsis Tactical Missile Aerodynamics by :

Download or read book Tactical Missile Aerodynamics written by and published by . This book was released on 1992 with total page 731 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Innovation in Flight

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ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Innovation in Flight by : Joseph R. Chambers

Download or read book Innovation in Flight written by Joseph R. Chambers and published by . This book was released on 2005 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Missile Configuration Design

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ISBN 13 :
Total Pages : 304 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Missile Configuration Design by : S. S. Chin

Download or read book Missile Configuration Design written by S. S. Chin and published by . This book was released on 1961 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beskriver principperne i f.m. konstruktionen af styrede missiler.