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Book Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet transport Airplane at Mach Numbers from 0 40 to 1 20

Download or read book Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet transport Airplane at Mach Numbers from 0 40 to 1 20 written by Eugene N. Brooks and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0 50 to 1 19 of a Supersonic Transport Model with a Modified M Wing

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 Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1 10 scale Model of the Blue Scout Jr  at Mach Numbers from 0 40 to 1 03

Download or read book Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1 10 scale Model of the Blue Scout Jr at Mach Numbers from 0 40 to 1 03 written by Thomas C. Kelly and published by . This book was released on 1962 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Loading Characteristics at Mach Numbers from 0 80 to 1 20 of a 1 10 scale Three stage Scout Model

Download or read book Aerodynamic Loading Characteristics at Mach Numbers from 0 80 to 1 20 of a 1 10 scale Three stage Scout Model written by Thomas C. Kelly and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.

Book Aerodynamic Characteristics in Pitch and Sideslip of a 1 15 scale Model of the Scout Vehicle at a Mach Number of 2 01

Download or read book Aerodynamic Characteristics in Pitch and Sideslip of a 1 15 scale Model of the Scout Vehicle at a Mach Number of 2 01 written by Ross B. Robinson and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Transonic Aerodynamic Characteristics of a Horizontal Take Off and Horizontal Landing Recoverable Booster Concept with Upper Stages Arranged in Parallel

Download or read book Transonic Aerodynamic Characteristics of a Horizontal Take Off and Horizontal Landing Recoverable Booster Concept with Upper Stages Arranged in Parallel written by and published by . This book was released on 1962 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0 065 scale Model of a Four stage Rocket Configuration at Mach Numbers of 1 41 and 1 82

Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0 065 scale Model of a Four stage Rocket Configuration at Mach Numbers of 1 41 and 1 82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0 6 to 3 0 and Angles of Attack from 0 to 180 Deg

Download or read book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0 6 to 3 0 and Angles of Attack from 0 to 180 Deg written by William B. Baker (Jr.) and published by . This book was released on 1976 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation of Static Aerodynamic Characteristics of a 1 9 scale Model of a Project Mercury Capsule at Mach Numbers from 1 60 to 4 65

Download or read book Wind tunnel Investigation of Static Aerodynamic Characteristics of a 1 9 scale Model of a Project Mercury Capsule at Mach Numbers from 1 60 to 4 65 written by David S. Shaw and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: