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 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 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 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 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 Sonic boom Characteristics in the Extreme Near Field of a Complex Airplane Model at Mach Numbers of 1 5 1 8 and 2 5 written by Odell A. Morris and published by . This book was released on 1970 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Exploratory Investigation in a Ballistic Range of the Stability Derivatives of a Simple Airplane Configuration at Low Supersonic Speeds written by Charles E. DeRose and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Download or read book Wind tunnel Investigation of Sonic boom Characteristics of Two Simple Wing Models at Mach Numbers from 2 3 to 4 63 written by Davis S. Miller and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic area rule Design and Rocket propelled Flight Investigation of a Zero lift Straight wing body nacelle Configuration Between Mach Numbers 0 8 and 1 53 written by Sherwood Hoffman and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The supersonic-area-rule concept was applied to the design of a straight-wing-body combination with large symmetrically mounted nacelles located at the 70-percent-semispan station. Both the nacelles and fuselage were indented to give a smooth total area distribution at a design Mach number of 1.41. The model was a zero-lift rocket-propelled vehicle and covered a continuous range of Mach number from 0.8 to 1.53 with corresponding Reynolds number from 3,000,000 to 4,000,000, based on wing mean aerodynamic chord. Also tested were two small equivalent bodies of revolution for Mach number 1.0 (which were propelled from a helium gun) of the basic wing-body combination.
Download or read book Toward Mach 2 written by J. D. Hunley and published by . This book was released on 1999 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Investigation of the Supersonic Area Rule for a Straight Wing body Configuration at Mach Numbers Between 0 8 and 1 5 written by Sherwood Hoffman and published by . This book was released on 1955 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic area rule Design and Rocket propelled Flight Investigation of a Zero lift Straight wing body nacelle Configuration Between Mach Numbers 0 8 and 1 53 written by Sherwood Hoffman and published by . This book was released on 1956 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: The supersonic-area-rule concept was applied to the design of a straight-wing-body combination with large symmetrically mounted nacelles located at the 70-percent-semispan station. Both the nacelles and fuselage were indented to give a smooth total area distribution at a design Mach number of 1.41. The model was a zero-lift rocket-propelled vehicle and covered a continuous range of Mach number from 0.8 to 1.53 with corresponding Reynolds number from 3,000,000 to 4,000,000, based on wing mean aerodynamic chord. Also tested were two small equivalent bodies of revolution for Mach number 1.0 (which were propelled from a helium gun) of the basic wing-body combination.
Download or read book Results from an Investigation in Rough Air at Mach Numbers from 0 84 to 1 67 of a Tailless Rocket Model Having 60 Degree Triangular Wings written by A. James Vitale and published by . This book was released on 1956 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results from a flight investigation in continuous rough air at Mach numbers from 0.54 to 1.67 are presented for a tailless rocket model having cruciform 60 degree triangular wings. The variation of root-mean-square acceleration increment with Mach number indicated a rapid increase of roughly 100 percent as the Mach number increased from 0.90 to 1.00. Of this 100 percent, about 70 percent appeared to be associated with the rapid decrease in pitch damping over this Mach number range. From Mach numbers 1.02 to 1.67, the experimental data showed little variation with Mach number at least within the estimated accuracy of the results of plus or minus 20 percent.
Download or read book Investigation of the Low subsonic Flight Characteristics of a Model of a Supersonic Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by Peter C. Boisseau and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation at Mach Numbers from 0 20 to 4 63 of the Aerodynamic Performance Static Stability and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight written by and published by . This book was released on 1961 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Beyond Tube and Wing written by Bruce Larrimer and published by . This book was released on 2020-06-15 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
