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Study Of The Stability And Drag At Mach Numbers From 45 To 135 Of A Conical Venus Entry Body
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Book Synopsis Study of the Stability and Drag at Mach Numbers from 4.5 to 13.5 of a Conical Venus-entry Body by : Peter F. Intrieri
Download or read book Study of the Stability and Drag at Mach Numbers from 4.5 to 13.5 of a Conical Venus-entry Body written by Peter F. Intrieri and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range by : Amado A. Trujillo
Download or read book Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range written by Amado A. Trujillo and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Stability and Drag Characteristics of Three Low-drag Reentry Bodies Obtained with Free-flight Models at Mach Numbers Between 5.0 and 7.0 by : Waldo L. Dickens
Download or read book Stability and Drag Characteristics of Three Low-drag Reentry Bodies Obtained with Free-flight Models at Mach Numbers Between 5.0 and 7.0 written by Waldo L. Dickens and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 by : Harvey A. Wallskog
Download or read book Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Drag Characteristics of Two Low-drag Reentry Bodies Obtained with Free-flight Models at Mach Numbers Between 0.96 and 3.28 by :
Download or read book Stability and Drag Characteristics of Two Low-drag Reentry Bodies Obtained with Free-flight Models at Mach Numbers Between 0.96 and 3.28 written by and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Reynolds Number Effects for a Series of Cone-cylinder Bodies at Mach Number of 1.62, 1.93, and 2.41 by : Carl E. Grigsby
Download or read book Investigation of Reynolds Number Effects for a Series of Cone-cylinder Bodies at Mach Number of 1.62, 1.93, and 2.41 written by Carl E. Grigsby and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An investigation of the Reynolds number for transition and the skin-friction drag at zero lift of eight cone-cylinder bodies having varying fineness ratios has been made at Mach numbers of 1.62, 1.93, and 2.41 over a Reynolds number range from 0.3 x 106 to 10 x 106. The accuracy of the skin-friction data was not sufficient to permit any general conclusions to be drawn. The Reynolds number for transition was found to be dependent upon both the tunnel stagnation pressure and Mach number.
Book Synopsis Experimental Stability and Control Results at Mach 19 of an Entry Vehicle Designed for an Intermediate Lift-drag Ratio by : Patrick J. Johnston
Download or read book Experimental Stability and Control Results at Mach 19 of an Entry Vehicle Designed for an Intermediate Lift-drag Ratio written by Patrick J. Johnston and published by . This book was released on 1968 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 by : Ralph W. Holtzclaw
Download or read book Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 written by Ralph W. Holtzclaw and published by . This book was released on 1962 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17 by :
Download or read book Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17 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 An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 to 1.8 by : A. Stanbrook
Download or read book An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 to 1.8 written by A. Stanbrook and published by . This book was released on 1968 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body Shape on the Drag of a 45 Degree Sweptback-wing-body Configuration at Mach Numbers from 0.90 to 1.43 by : Walter B. Olstad
Download or read book Effects of Body Shape on the Drag of a 45 Degree Sweptback-wing-body Configuration at Mach Numbers from 0.90 to 1.43 written by Walter B. Olstad and published by . This book was released on 1958 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics from Mach 1.50 to 2.86 of a Lifting Entry Vehicle Alone, with Adapter Sections, and with a Saturn Launch Vehicle by :
Download or read book Aerodynamic Characteristics from Mach 1.50 to 2.86 of a Lifting Entry Vehicle Alone, with Adapter Sections, and with a Saturn Launch Vehicle written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Reynolds Number on the Stability of a Blunt-nosed Flared Cylinder from Mach 17.6 to 22.2 in Helium by :
Download or read book Effects of Reynolds Number on the Stability of a Blunt-nosed Flared Cylinder from Mach 17.6 to 22.2 in Helium written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
