A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 PDF full book. Access full book title A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 by James A. Humphrey. Download full books in PDF and EPUB format.

A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0

A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 PDF Author: James A. Humphrey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 234

Book Description
Wrap-around fin effectiveness for tube-launched missiles was investigated in a series of 6 wind tunnel tests. Wind tunnels were AEDC Propulsion Wind Tunnel, NASA/Langley Research Center Unitary Plan Wind Tunnel and McDonnell Douglas 4-foot Trisonic Wind Tunnel. Mach number range was 0.3 to 3.0. Basic model was a 2-caliber secant ogive nose with an 8-caliber cylindrical afterbody and 21 fin configurations. Variations in the coefficients are presented for changes in fin geometry including taper ratio and leading edge sweep angle, aspect ratio, exposed semi-span, and root chord length; opening angle, fully closed to 10 deg past fully open; and body step down.

A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0

A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 PDF Author: James A. Humphrey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 234

Book Description
Wrap-around fin effectiveness for tube-launched missiles was investigated in a series of 6 wind tunnel tests. Wind tunnels were AEDC Propulsion Wind Tunnel, NASA/Langley Research Center Unitary Plan Wind Tunnel and McDonnell Douglas 4-foot Trisonic Wind Tunnel. Mach number range was 0.3 to 3.0. Basic model was a 2-caliber secant ogive nose with an 8-caliber cylindrical afterbody and 21 fin configurations. Variations in the coefficients are presented for changes in fin geometry including taper ratio and leading edge sweep angle, aspect ratio, exposed semi-span, and root chord length; opening angle, fully closed to 10 deg past fully open; and body step down.

Heat Transfer from Cylinders Having Closely Spaced Fins

Heat Transfer from Cylinders Having Closely Spaced Fins PDF Author: Arnold E. Biermann
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 622

Book Description
The use of baffles for directing the air around the cylinders with closely spaced fins proved very effective in increasing the over-all heat-transfer coefficient provided that the spacing was not appreciably less than that for maximum heat transfer.

Fins into Limbs

Fins into Limbs PDF Author: Brian K. Hall
Publisher: University of Chicago Press
ISBN: 0226313409
Category : Science
Languages : en
Pages : 461

Book Description
Long ago, fish fins evolved into the limbs of land vertebrates and tetrapods. During this transition, some elements of the fin were carried over while new features developed. Lizard limbs, bird wings, and human arms and legs are therefore all evolutionary modifications of the original tetrapod limb. A comprehensive look at the current state of research on fin and limb evolution and development, this volume addresses a wide range of subjects—including growth, structure, maintenance, function, and regeneration. Divided into sections on evolution, development, and transformations, the book begins with a historical introduction to the study of fins and limbs and goes on to consider the evolution of limbs into wings as well as adaptations associated with specialized modes of life, such as digging and burrowing. Fins into Limbs also discusses occasions when evolution appears to have been reversed—in whales, for example, whose front limbs became flippers when they reverted to the water—as well as situations in which limbs are lost, such as in snakes. With contributions from world-renowned researchers, Fins into Limbs will be a font for further investigations in the changing field of evolutionary developmental biology.

Automotive Industries

Automotive Industries PDF Author:
Publisher:
ISBN:
Category : Aircraft industry
Languages : en
Pages : 1666

Book Description


Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30

Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 PDF Author: D.K. Smith
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 166

Book Description


Reports and Memoranda

Reports and Memoranda PDF Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 166

Book Description
Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

Reports and Memoranda

Reports and Memoranda PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 604

Book Description


Annual Report ... Including Technical Reports ...

Annual Report ... Including Technical Reports ... PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 734

Book Description


Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 648

Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements

A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements PDF Author: Carl Kaplan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252

Book Description