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Investigation Of The Aerodynamic And Control Characteristics Of A Hypersonic Glider At Mach Numbers From 166 To 465
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Book Synopsis Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65 by :
Download or read book Investigation of the Aerodynamic and Control Characteristics of a Hypersonic Glider at Mach Numbers from 1.66 to 4.65 written by and published by . This book was released on 1961 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers by : Alvin Seiff
Download or read book Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers written by Alvin Seiff and published by . This book was released on 1961 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 by : William John Small
Download or read book Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 written by William John Small and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 by : Walter P. Nelms
Download or read book Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 written by Walter P. Nelms and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The configuration had a delta planform with an elliptic cone forebody and an afterbody of elliptic cross section. Detailed effects of varying angle of attack (-2 to 15 deg), angle of sideslip (-2 to 8 deg), Mach number, and configuration buildup were considered. In addition, the effectiveness of horizontal tail, vertical tail, and canard stabilizing and control surfaces was investigated. The results indicate that all configurations were longitudinally stable near maximum lift drag ratio. The configurations with vertical tails were directionally stable at all angles of attack. Trim penalties were small at hypersonic speeds for a center of gravity location representative of the airplane, but because of the large rearward travel of the aerodynamic center, trim penalties were severe at transonic Mach numbers.
Book Synopsis A Transonic Wind-tunnel Investigation of the Static Longitudinal and Lateral Aerodynamic Characteristics of a Proposed Hypersonic Glider with Several Booster Configurations by : Ralph P. Bielat
Download or read book A Transonic Wind-tunnel Investigation of the Static Longitudinal and Lateral Aerodynamic Characteristics of a Proposed Hypersonic Glider with Several Booster Configurations written by Ralph P. Bielat and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2 by :
Download or read book Aerodynamic Characteristics of a Hypersonic Glider Configuration at Mach Numbers from 0.6 to 3.2 written by and published by . This book was released on 1964 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 by : James C. Ellison
Download or read book Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 written by James C. Ellison and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Also available online.
Book Synopsis The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4 by : Stuart L. Treon
Download or read book The Effects of Wing Plan Form on the Static Longitudinal Aerodynamic Characteristics of a Flat-top Hypersonic Aircraft at Mach Numbers from 0.6 to 1.4 written by Stuart L. Treon and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds by :
Download or read book Investigation of the Low Subsonic Stability and Control Characteristics of a Model of a Hypersonic Boost-glide Airplane Designed for High Lift-drag Ratios at Low Speeds written by and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Plan Form Geometry on the Aerodynamic Characteristics of a Hypersonic Glider at Mach Numbers Up to 9.6 by : Charles L. Ladson
Download or read book Effects of Wing Plan Form Geometry on the Aerodynamic Characteristics of a Hypersonic Glider at Mach Numbers Up to 9.6 written by Charles L. Ladson and published by . This book was released on 1960 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Measurement at Mach 19 for a Winged Re-entry Configuration by : Stavros A. Hartofilis
Download or read book Pressure Measurement at Mach 19 for a Winged Re-entry Configuration written by Stavros A. Hartofilis and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Subsonic Investigation of the Aerodynamic Characteristics of a Hypersonic Glider Model with and Without Deflected Elevons and Body Flap by :
Download or read book High Subsonic Investigation of the Aerodynamic Characteristics of a Hypersonic Glider Model with and Without Deflected Elevons and Body Flap written by and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Hypersonic Flow Separation and Its Effects on Aerodynamic Control Characteristics by : Douglas Eugene Abbott
Download or read book Investigation of Hypersonic Flow Separation and Its Effects on Aerodynamic Control Characteristics written by Douglas Eugene Abbott and published by . This book was released on 1962 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of the present study is to investigate laminar separation at hypersonic speeds, especially as it affects aerodynamic control characteristcis. Theoretical methods for use with computing machines hae been developed for calculating the pressure distribution due to laminar separation of the free-interaction type upstream and downstream of the separation point. The theories account for effects of Mach number, Reynolds number, wall heating and cooling, and specific heat ratio and show significant effects of all these parameters on separation. An experimental investigation was made of flare-cylinder combination with extensive separation at Mach numbers 4 and 6, Reynolds numbers of 10(3) to 10(4), and for adiabatic and cooled walls. In general, the separation was not of the free-interaction type so that modifications of the theory are required to adapt it to this type of separation. Methods for making such modifications are discussed together with methods for computing hypersonic control characteristics for various cases of seaparated flows.
Book Synopsis Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by by : John W. Paulson
Download or read book Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by written by John W. Paulson and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52 by :
Download or read book Aerodynamic and Stability Characteristics of a Proposed Hypersonic Glider-booster Combination at Mach Numbers from 0.60 to 3.52 written by and published by . This book was released on 1964 with total page 78 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 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
