Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and a 40 Sweepback written by John P. Gapcynski and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degrees Sweepback Static Lateral Control Characteristics at Mach Number of 1 40 and 1 59 written by Ross B. Robinson and published by . This book was released on 1950 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degrees Sweepback Static Lateral Stability Characteristics at Mach Numbers of 1 40 and 1 59 written by M. Leroy Spearman and published by . This book was released on 1950 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by M. Leroy Spearman and published by . This book was released on 1954 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a supersonic aircraft configuration equipped with a canard control surface (in addition to a rearward horizontal stabilizer) at a Mach number of 1.89. The model had a 40 degree sweptback tapered wing with an aspect ratio of 4 and 10-percent-thick circular-arc sections normal to the quarter-chord line. The canard surface had a total area about 0ne-twelfth of the total wing area and was located 2.27 mean aerodynamic chord lengths ahead of the reference center of gravity.

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by John P. Gapcynski and published by . This book was released on 1952 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Section and 40 Degrees Sweepback a Pressure distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1 40 written by Norman F. Smith and published by . This book was released on 1951 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by Norman F. Smith and published by . This book was released on 1951 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt: A force investigation of a supersonic aircraft configuration and various combinations of its components has been conducted in the Langley 4- by 4-foot supersonic tunnel. The tests were performed at Mach numbers of 1.40 and 1.59 at a Reynolds number of approximately 600,000 based on the wing mean aerodynamic chord and are a part of an extensive investigation of the force and pressure-distribution characteristics of this configuration.

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by Morton Cooper and published by . This book was released on 1950 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by Frederick C. Grant and published by . This book was released on 1952 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degrees Sweepback Static Longitudinal Stability and Control Characteristics at a Mach Number of 1 59 written by M. Leroy Spearman and published by . This book was released on 1950 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback written by Clyde V. Hamilton and published by . This book was released on 1954 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel at a Mach number of 1.61 to determine the stability of control characteristics of a supersonic aircraft configuration with a 40 percent sweptback wing and equipped with spoiler lateral control devices. Some effects of various types of spoilers, spoiler span, projection, and chordwise location were investigated, as well as the hinge-moment characteristics for a plain spoiler.

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and 40 Degree Sweepback Static Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1 89 written by M. Leroy Spearman and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Results of the Flight Investigation Between Mach Numbers of 0 80 and 1 36 of a Rocket powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular arc Sections and 40 Sweepback written by Charles T. D'Aiutolo and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Curcular arc Sections and 40 Degrees Sweepback written by M. Leroy Spearman and published by . This book was released on 1950 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Results of the Flight Investigation Between Mach Numbers of 0 80 and 1 36 of a Rocket powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular arc Sections and 40 Degrees Sweepback written by Charles T. D'Aiutolo and published by . This book was released on 1950 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Laboratory Report LR written by National Aeronautical Establishment (Canada) and published by . This book was released on 1958 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt: