Plume Interference Effects on Missile Bodies

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

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Book Synopsis Plume Interference Effects on Missile Bodies by : S. Raghunathan

Download or read book Plume Interference Effects on Missile Bodies written by S. Raghunathan and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Plume Interference Effects on Missile Bodies at Supersonic Speeds

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (593 download)

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Book Synopsis Plume Interference Effects on Missile Bodies at Supersonic Speeds by : Y. K. Lee

Download or read book Plume Interference Effects on Missile Bodies at Supersonic Speeds written by Y. K. Lee and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 by : Reino J. Salmi

Download or read book Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 written by Reino J. Salmi and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1982 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Plume Interference Effect on Missile Bodies and Control

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

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Book Synopsis Plume Interference Effect on Missile Bodies and Control by : Y. K. Lee

Download or read book Plume Interference Effect on Missile Bodies and Control written by Y. K. Lee and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Aeronautical Journal

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

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Book Synopsis The Aeronautical Journal by :

Download or read book The Aeronautical Journal written by and published by . This book was released on 2004 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 392 pages
Book Rating : 4.:/5 (319 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 1960 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of Flow and Stability Characteristics for a Body of Revolution with Fins and Flare in Presence of Plume Induced Separation at Mach Numbers 0.7 to 1.4

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ISBN 13 :
Total Pages : 200 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Investigation of Flow and Stability Characteristics for a Body of Revolution with Fins and Flare in Presence of Plume Induced Separation at Mach Numbers 0.7 to 1.4 by : Calvin Wayne Dahlke

Download or read book An Investigation of Flow and Stability Characteristics for a Body of Revolution with Fins and Flare in Presence of Plume Induced Separation at Mach Numbers 0.7 to 1.4 written by Calvin Wayne Dahlke and published by . This book was released on 1977 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of a wind tunnel test, simulating rocket motor exhaust jet effects on missile aerodynamic at Mach numbers of 0.7 to 1.4 are presented. A normal jet plume simulator was used to induce afterbody boundary layer separation. Flow visualization techniques including both shadowgraph and oil flow photographs were taken. The primary emphasis for this report is the force and moment measurements taken on twelve configurations including: five tail fin configurations; body alone; three forward fin configurations; body flare combination; and two combinations of forward fins/strakes with tail fins. All force and moment coefficients are presented in plotted form. One configuration is shown with ground plane interference simulation. (Author).

41st AIAA Aerospace Sciences Meeting & Exhibit

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ISBN 13 :
Total Pages : 580 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 41st AIAA Aerospace Sciences Meeting & Exhibit by :

Download or read book 41st AIAA Aerospace Sciences Meeting & Exhibit written by and published by . This book was released on 2003 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Axisymmetric and Normal Air Jet Plumes and Solid Plume on Cylindrical Afterbody Pressure Distributions at Mach Numbers from 1.65 to 2.50

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Axisymmetric and Normal Air Jet Plumes and Solid Plume on Cylindrical Afterbody Pressure Distributions at Mach Numbers from 1.65 to 2.50 by : Peter F. Covell

Download or read book Effects of Axisymmetric and Normal Air Jet Plumes and Solid Plume on Cylindrical Afterbody Pressure Distributions at Mach Numbers from 1.65 to 2.50 written by Peter F. Covell and published by . This book was released on 1982 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Research in Progress

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ISBN 13 :
Total Pages : 604 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Research in Progress by :

Download or read book Research in Progress written by and published by . This book was released on 1976 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of the Effectiveness of Several Devices in Simulating a Rocket Plume at Free Stream Mach Numbers 0.9 to 1.2

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Investigation of the Effectiveness of Several Devices in Simulating a Rocket Plume at Free Stream Mach Numbers 0.9 to 1.2 by : James Robert Burt (Jr.)

Download or read book An Investigation of the Effectiveness of Several Devices in Simulating a Rocket Plume at Free Stream Mach Numbers 0.9 to 1.2 written by James Robert Burt (Jr.) and published by . This book was released on 1971 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effectiveness of several devices in simulating the effects of a rocket plume on the flow field of a typical missile in the transonic Mach number range was investigated. Two plume-shaped solid bodies and three step-type plume simulators were tested. The effects on model pressure distribution of small angle of attack and plume-simulator position were investigated. The analysis showed that all the plume simulators tested can give approximately the same model afterbody pressure distribution at transonic Mach numbers and small angles of attack as an actual rocket plume. (Author).

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 992 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 992 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Jet Pluming on the Static Stability of Five Rocket Models at Mach Numbers of 4, 5, and 6 and Static Pressure Ratios Up to 26 000

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ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Jet Pluming on the Static Stability of Five Rocket Models at Mach Numbers of 4, 5, and 6 and Static Pressure Ratios Up to 26 000 by : William F. Hinson

Download or read book Effects of Jet Pluming on the Static Stability of Five Rocket Models at Mach Numbers of 4, 5, and 6 and Static Pressure Ratios Up to 26 000 written by William F. Hinson and published by . This book was released on 1967 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 538 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 1995 with total page 538 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.

Space Shuttle Technical Conference, Part 1

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ISBN 13 :
Total Pages : 604 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Space Shuttle Technical Conference, Part 1 by :

Download or read book Space Shuttle Technical Conference, Part 1 written by and published by . This book was released on 1985 with total page 604 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Missile Aerodynamics

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Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 : 9780962062902
Total Pages : 450 pages
Book Rating : 4.0/5 (629 download)

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Book Synopsis Missile Aerodynamics by : Jack Norman Nielsen

Download or read book Missile Aerodynamics written by Jack Norman Nielsen and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988-01-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.