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Experimental Investigation Of Longitudinal Static Stability Of A Glider And 11 Booster Configurations At Mach Numbers From 162 To 686
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Book Synopsis Experimental Investigation of Longitudinal Static Stability of a Glider and 11 Booster Configurations at Mach Numbers from 1.62 to 6.86 by :
Download or read book Experimental Investigation of Longitudinal Static Stability of a Glider and 11 Booster Configurations at Mach Numbers from 1.62 to 6.86 written by and published by . This book was released on 1961 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Stability and Control Characteristics and Pressure Distrubutions of a Model of a Hypersonic Glider in Combination with Each of Two Booster Systems at Mach Numbers of 1.80, 2.75, and 4.50 by :
Download or read book Investigation of the Static Stability and Control Characteristics and Pressure Distrubutions of a Model of a Hypersonic Glider in Combination with Each of Two Booster Systems at Mach Numbers of 1.80, 2.75, and 4.50 written by and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01 by : Gerald V. Foster
Download or read book Static Stability Characteristics of a Series of Hypersonic Boost-glide Configurations at Mach Numbers of 1.41 and 2.01 written by Gerald V. Foster and published by . This book was released on 1959 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability Characteristics of a Blunted Glider Reentry Configuration Having 79.5° Sweepback and 45° Dihedral at Mach Number of 6.2 and Angles of Attack Up to 20° by : Edward E. Mayo
Download or read book Static Longitudinal Stability Characteristics of a Blunted Glider Reentry Configuration Having 79.5° Sweepback and 45° Dihedral at Mach Number of 6.2 and Angles of Attack Up to 20° written by Edward E. Mayo and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Stability and Control Characteristics and Pressure Distributions of a Model of a Hypersonic Glider in Combination with Each of Two Booster Systems at Mach Numbers of 1.80, 2.75, and 4.50 by : Robert M. Lust
Download or read book Investigation of the Static Stability and Control Characteristics and Pressure Distributions of a Model of a Hypersonic Glider in Combination with Each of Two Booster Systems at Mach Numbers of 1.80, 2.75, and 4.50 written by Robert M. Lust and published by . This book was released on 1961 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics at a Mach Number of 1.89 of a Lightweight Glider Reentry Configuration by : Ross B. Robinson
Download or read book Stability and Control Characteristics at a Mach Number of 1.89 of a Lightweight Glider Reentry Configuration written by Ross B. Robinson and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Dynamic Stability of a Towed Parawing Glider Model by : Robert E. Shanks
Download or read book Experimental Investigation of the Dynamic Stability of a Towed Parawing Glider Model written by Robert E. Shanks and published by . This book was released on 1963 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability Characteristics of a Blunted Glider Reentry Configuration Having 79.5 Sweep and 45 Dihedral at a Mach Number of 6.2 and Angles of Attack Up to 20 by : Edward E. Mayo
Download or read book Static Longitudinal Stability Characteristics of a Blunted Glider Reentry Configuration Having 79.5 Sweep and 45 Dihedral at a Mach Number of 6.2 and Angles of Attack Up to 20 written by Edward E. Mayo and published by . This book was released on 1959 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Control Characteristics of a Glider Reentry Configuration Having 79.5 Deg Sweepback and 45 Deg Dihedral at a Mach Number of 6.01 by :
Download or read book Static Control Characteristics of a Glider Reentry Configuration Having 79.5 Deg Sweepback and 45 Deg Dihedral at a Mach Number of 6.01 written by and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability Characteristics of Blunted Glider Reentry Configuration Having 79.5° Sweepback and 45° Dihedral at Mach Number of 6.2 and Angles of Attack Up to 20° [with List of References] by :
Download or read book Static Longitudinal Stability Characteristics of Blunted Glider Reentry Configuration Having 79.5° Sweepback and 45° Dihedral at Mach Number of 6.2 and Angles of Attack Up to 20° [with List of References] written by and published by . This book was released on 1959 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies by : William Letko
Download or read book Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies written by William Letko and published by . This book was released on 1960 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations by :
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations written by and published by . This book was released on 1960 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Estimation of Static Longitudinal Stability of Aircraft Configurations at High Mach Numbers and at Angles of Attack Between 0 Degrees and 180 Degrees by : Duane W. Dugan
Download or read book Estimation of Static Longitudinal Stability of Aircraft Configurations at High Mach Numbers and at Angles of Attack Between 0 Degrees and 180 Degrees written by Duane W. Dugan and published by . This book was released on 1959 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lateral Stability Investigation at Mach Numbers from 0.8 to 1.7 of Two Rocket-boosted Models of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail by : John C. McFall
Download or read book Lateral Stability Investigation at Mach Numbers from 0.8 to 1.7 of Two Rocket-boosted Models of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail written by John C. McFall and published by . This book was released on 1957 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rocket-boosted free-flight tests of two models of an airplane configuration having a 45 degree swept wing and a low horizontal-tail position have provided lateral stability derivatives and control effectiveness data for a Mach number range from 0.8 to 1.7. The experimental lateral stability derivatives presented are corrected to rigid conditions and compared with theoretically calculated rigid derivatives. The results are presented without detailed analysis.
Book Synopsis Lift, Drag, and Static Longitudinal Stability Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28 by : Stanford E. Neice
Download or read book Lift, Drag, and Static Longitudinal Stability Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28 written by Stanford E. Neice and published by . This book was released on 1955 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability Investigation for a Mach Number Range of 0.8 to 1.7 of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail by : John C. McFall
Download or read book Longitudinal Stability Investigation for a Mach Number Range of 0.8 to 1.7 of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail written by John C. McFall and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An airplane configuration model having a 45 degree swept wing of aspect ratio 4.0 and taper ratio of 0.3 with a low swept horizontal tail has been flown in a longitudinal stability investigation over a Mach number range of 0.8 to 1.7. Longitudinal aerodynamic coefficients and stability derivatives for the configuration are presented as functions of Mach number over the test range. Comparisons of lift-curve slopes are made with wind-tunnel data and comparisons of tail effectiveness are made with rocket-model data, and show generally good agreement. Absence of an unstable break in the pitching-moment curve, usually associated with this wing, indicates a favorable location of the horizontal tail for the lift and Mach number range of the investigation.
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration by : David E. Fetterman
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration written by David E. Fetterman and published by . This book was released on 1960 with total page 87 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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