Aerodynamic Characteristics of Two Trailblazer II Blunted 9 Degree Cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of Two Trailblazer II Blunted 9 Degree Cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium by : Herbert R. Schippell

Download or read book Aerodynamic Characteristics of Two Trailblazer II Blunted 9 Degree Cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium written by Herbert R. Schippell and published by . This book was released on 1965 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Two Trailblazer II Blunted 9 ̊cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (249 download)

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Book Synopsis Aerodynamic Characteristics of Two Trailblazer II Blunted 9 ̊cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium by : Herbert R. Schippell

Download or read book Aerodynamic Characteristics of Two Trailblazer II Blunted 9 ̊cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium written by Herbert R. Schippell and published by . This book was released on 1965 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 by : George C. Kenyon

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 written by George C. Kenyon and published by . This book was released on 1961 with total page 54 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:

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

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

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Book Synopsis THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 by :

Download or read book THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 written by and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Determination of Aerodynamic Drag on a Blunted 10-deg Cone at Angles of Attack in Hypersonic, Rarefied Flow

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

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Book Synopsis Experimental Determination of Aerodynamic Drag on a Blunted 10-deg Cone at Angles of Attack in Hypersonic, Rarefied Flow by : David E. Boylan

Download or read book Experimental Determination of Aerodynamic Drag on a Blunted 10-deg Cone at Angles of Attack in Hypersonic, Rarefied Flow written by David E. Boylan and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Characteristics of an Aerodynamic Control System for Use with Blunt Entry Configurations at Mach Numbers of 10.7 and 21.2 in Helium

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Characteristics of an Aerodynamic Control System for Use with Blunt Entry Configurations at Mach Numbers of 10.7 and 21.2 in Helium by :

Download or read book Characteristics of an Aerodynamic Control System for Use with Blunt Entry Configurations at Mach Numbers of 10.7 and 21.2 in Helium written by and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 by :

Download or read book Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 written by and published by . This book was released on 1963 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90

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

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 by :

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 written by and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7

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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 Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7 by : William O. Armstrong

Download or read book Aerodynamic Characteristics of a Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7 written by William O. Armstrong and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6

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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 Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 by : Michael F. Sarabia

Download or read book Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 written by Michael F. Sarabia and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane

Download or read book Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 written by Lucille C. Coltrane and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel

Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.

Aerodynamic Characteristics of Two Winged Reentry Vehicles at Supersonic and Hypersonic Speeds

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics of Two Winged Reentry Vehicles at Supersonic and Hypersonic Speeds by :

Download or read book Aerodynamic Characteristics of Two Winged Reentry Vehicles at Supersonic and Hypersonic Speeds written by and published by . This book was released on 1961 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

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ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.:/5 (76 download)

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Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 by : George C. Kenyon

Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 written by George C. Kenyon and published by . This book was released on 1961 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63

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ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (79 download)

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Book Synopsis Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 by : Gerald V. Foster

Download or read book Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 written by Gerald V. Foster and published by . This book was released on 1968 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg by :

Download or read book Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg written by and published by . This book was released on 1985 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: