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Book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II Apollo Test Vehicle at Mach Numbers from 0 056 to 4 65

Download or read book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II Apollo Test Vehicle at Mach Numbers from 0 056 to 4 65 written by Robert H. Moore and published by . This book was released on 1968 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Stability and Control Characteristics of a 0 030 scale Model of a Little Joe 2 Apollo Space Vehicle at Mach Numbers from 1 57 to 4 65

Download or read book Static Stability and Control Characteristics of a 0 030 scale Model of a Little Joe 2 Apollo Space Vehicle at Mach Numbers from 1 57 to 4 65 written by and published by . This book was released on 1963 with total page 28 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 Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 20 of a Variable wing sweep STOL Configuration

Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 20 of a Variable wing sweep STOL Configuration written by Gerald V. Foster and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Aerodynamic Characteristics of Several Wing and Blunt body Shapes Applicable for Use as Reentry Configurations at a Mach Number of 6 8 and Angles of Attack Up to 90

Download or read book Static Longitudinal Aerodynamic Characteristics of Several Wing and Blunt body Shapes Applicable for Use as Reentry Configurations at a Mach Number of 6 8 and Angles of Attack Up to 90 written by Jim A. Penland and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations

Download or read book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.

Book Wing on and Wing off Longitudinal Characteristics of an Airplane Configuration Having a Thin Unswept Wing of Aspect Ratio 3 as Obtained from Rocket propelled Models at Mach Numbers from 0 8 to 1 4

Download or read book Wing on and Wing off Longitudinal Characteristics of an Airplane Configuration Having a Thin Unswept Wing of Aspect Ratio 3 as Obtained from Rocket propelled Models at Mach Numbers from 0 8 to 1 4 written by Clarence L. Gillis and published by . This book was released on 1959 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics of a Model Airplane Configuration Equipped with a Scaled X 1 Airplane Wing

Download or read book Longitudinal Aerodynamic Characteristics of a Model Airplane Configuration Equipped with a Scaled X 1 Airplane Wing written by James H. Parks and published by . This book was released on 1952 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Static Longitudinal Aerodynamic Characteristics of a Right Triangular Pyrimidal Lifting Reentry Configuration at Mach Numbers of 3 00 4 50 and 6 00 for Angles of Attack Up to 56

Download or read book Static Longitudinal Aerodynamic Characteristics of a Right Triangular Pyrimidal Lifting Reentry Configuration at Mach Numbers of 3 00 4 50 and 6 00 for Angles of Attack Up to 56 written by Dewey E. Wornom and published by . This book was released on 1962 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: