Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 ̊in Helium

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 ̊in Helium by : Dal V. Maddalon

Download or read book Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 ̊in Helium written by Dal V. Maddalon and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 Degrees in Helium

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 Degrees in Helium by : Dal V. Maddalon

Download or read book Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 Degrees in Helium written by Dal V. Maddalon and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack

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ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack by : Joseph L. Sims

Download or read book Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1973 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.

Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20 by : Theodore R. Creel

Download or read book Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20 written by Theodore R. Creel and published by . This book was released on 1968 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 by : Jim A. Penland

Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 written by Jim A. Penland and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

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

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Book Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman

Download or read book Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium written by Melvin J. Fohrman and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Raked-off Circular and Elliptical Cones at a Mach Number of 20 in Helium

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of Raked-off Circular and Elliptical Cones at a Mach Number of 20 in Helium by : John K. Molloy

Download or read book Aerodynamic Characteristics of Raked-off Circular and Elliptical Cones at a Mach Number of 20 in Helium written by John K. Molloy and published by . This book was released on 1966 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21 by :

Download or read book Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21 written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees by : JIM A. PENLAND

Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees written by JIM A. PENLAND and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force tests of a series of right circular cones having semivertex angles ranging from 5 to 45 degrees and a series of right circular cone-cylinder configurations having semivertex angles ranging from 5 to 20 degrees and an afterbody fineness ratio of 6 have been made in the Langley 11inch hypersonic tunnel at a Mach number of 6.83, a Reynolds number of 0.24 x 10 to the 6th power per inch, and angles of attack up to 130 degrees. An analysis of the results made use of the Newtonian and modified Newtonian theories and the exact theory. A comparison of the experimental data of both cone and cone-cylinder configurations with theoretical calculations shows that the Newtonian concept gives excellent predictions of trends of the force characteristics and the locations with respect to angle of attack of the points of maximum lift, maximum drag, and maximum lift-drag ratio. Both the Newtonian and exact theories give excellent predictions of the sign and value of the initial lift-curve slope. (Author).

Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium by : Joseph W. Cleary

Download or read book Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium written by Joseph W. Cleary and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects by : Dal V. Maddalon

Download or read book Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects written by Dal V. Maddalon and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Air-helium Simulation of the Aerodynamic Force Coefficients of Cones at Hypersonic Speeds

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Air-helium Simulation of the Aerodynamic Force Coefficients of Cones at Hypersonic Speeds by : Charles L. Ladson

Download or read book Air-helium Simulation of the Aerodynamic Force Coefficients of Cones at Hypersonic Speeds written by Charles L. Ladson and published by . This book was released on 1962 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section by :

Download or read book Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section written by and published by . This book was released on 1983 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Characteristics of Several Configurations at Hypersonic Mach Numbers in Conical and Contoured Nozzles

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Characteristics of Several Configurations at Hypersonic Mach Numbers in Conical and Contoured Nozzles by : James P. Arrington

Download or read book Longitudinal Characteristics of Several Configurations at Hypersonic Mach Numbers in Conical and Contoured Nozzles written by James P. Arrington and published by . This book was released on 1964 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees by : James L. Amick

Download or read book Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees written by James L. Amick and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a 10 Deg Sharp Cone at Hypersonic Speeds and High Angles of Attack

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ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Aerodynamic Characteristics of a 10 Deg Sharp Cone at Hypersonic Speeds and High Angles of Attack by :

Download or read book Aerodynamic Characteristics of a 10 Deg Sharp Cone at Hypersonic Speeds and High Angles of Attack written by and published by . This book was released on 1975 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flying instrumented model was tested in a hypersonic facility at M = 5.30, 6.34 and 9.94 and Re = 300,000 to 1,200,000 ft. Aerodynamic lift, total drag and base drag coefficients were obtained together with detailed base pressure distribution measurements at angles of attack from 0 to 60 deg. The measured lift and drag coefficients showed good agreement with the modified Newtonian theory. The centerline base pressure/free-stream static pressure, psia distribution was nearly independent of the angle of attack from -10 to -30 deg but increased rapidly for all test conditions beyond alpha = -30 deg. For similar conditions at angle of attack and Reynolds number, an increase in Mach number resulted in an increase of the base pressure ratio. The measurements indicated a highly complex base flow region, and tentative explanation of the observed results was offered.

A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases

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ISBN 13 :
Total Pages : 596 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases by : Sandia Corporation

Download or read book A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases written by Sandia Corporation and published by . This book was released on 1965 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt: