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Static Stability Investigation Of A Sounding Rocket Vehicle At Mach Numbers From 150 To 463
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Book Synopsis Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63 by : C. Donald Babb
Download or read book Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63 written by C. Donald Babb and published by . This book was released on 1967 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63 by : C. Donald Babb
Download or read book Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63 written by C. Donald Babb and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 by : James C. Ferris
Download or read book Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 written by James C. Ferris and published by . This book was released on 1967 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 by : James C. Ferris
Download or read book Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 written by James C. Ferris and published by . This book was released on 1967 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Statistic Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 by : James C. Ferris
Download or read book Statistic Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 written by James C. Ferris and published by . This book was released on 1967 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° by : J. W. Usry
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° written by J. W. Usry and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50 by : Kenneth L. Turner
Download or read book Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50 written by Kenneth L. Turner and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges by : Joseph A. Yuska
Download or read book Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges written by Joseph A. Yuska and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.
Book Synopsis Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180 Deg by :
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180 Deg written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigation of Proposed Project the Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigation of Proposed Project the Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability of a Rocket Vehicle Having a Rear-facing Step Ahead of the Stabilizing Fins by : Robert J. Keynton
Download or read book Static Longitudinal Stability of a Rocket Vehicle Having a Rear-facing Step Ahead of the Stabilizing Fins written by Robert J. Keynton and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to determine the static longitudinal stability characteristics of a fin-stabilized rocket-vehicle configuration which had a rearward facing step located upstream of the fins. Two fin sizes and planforms, a delta and a clipped delta, were tested. The angle of attack was varied from 6° to -6° and the Reynolds number based on model length was about 10 x 106. The configuration with the larger fins (clipped delta) had a center of pressure slightly rearward of and an initial normal-force-curve slope slightly higher than that of the configuration with the smaller fins (delta) as would be expected. Calculations of the stability parameters gave a slightly lower initial slope of the normal-force curve than measured data, probably because of boundary-layer separation ahead of the step. The calculated center of pressure agreed well with the measured data. Measured and calculated increments in the initial slope of the normal-force curve and in the center of pressure, due to changing fins, were in excellent agreement indicating that separated flow downstream of the step did not influence flow over the fins. This result was consistent with data from schlieren photographs."--P. 1.
Book Synopsis Investigation of the Static Longitudinal Stability Characteristics of a 0.067-scale Model of a Four-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 by : Lloyd S. Jernell
Download or read book Investigation of the Static Longitudinal Stability Characteristics of a 0.067-scale Model of a Four-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 written by Lloyd S. Jernell and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 by : Donald T. Gregory
Download or read book Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 written by Donald T. Gregory and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by : Clarence A. Brown
Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.10-scale Model of a Three-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 by : Lloyd S. Jernell
Download or read book Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.10-scale Model of a Three-stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65 written by Lloyd S. Jernell and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
