Download or read book The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane written by F. H. Norton and published by . This book was released on 1921 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane written by F. H. Norton and published by . This book was released on 1922 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane written by Frederick Harwood Norton and published by . This book was released on 1923 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Wings and Tail Surfaces of a PW 9 Pursuit Airplane in Flight written by A. M. Rothrock and published by . This book was released on 1930 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane written by F. H. Norton and published by . This book was released on 1921 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Horizontal Tail Surfaces of an Airplane written by F. H. Norton and published by . This book was released on 1921 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution of a 0 0667 scale Model of the X 15 Airplane for an Angle of attack Range of 0 to 28 at Mach Numbers of 2 30 288 and 4 65 written by B. Leon Hodge and published by . This book was released on 1960 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over a Semicircular Wing Tip on a Biplane in Flight written by Richard V. Rhode and published by . This book was released on 1931 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped with a semicircular wing tip. The results are given in tables and curves in such form that the load distribution for any normal force coefficient within the usual range encountered in flight may easily be determined.
Download or read book The Pressure Distribution Over the Horizontal and Vertical Tail Surfaces of the F6C 4 Pursuit Airplane in Violent Maneuvers written by Richard V. Rhode and published by . This book was released on 1929 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller driven Pursuit Airplane in Flight written by Melvin Sadoff and published by . This book was released on 1947 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements were made in sideslipping flight at a Mach number of 0.50 of the pressure distribution over the horizontal tail surfaces of a tractor-propeller-driven pursuit airplane, to determine the effects of angle of sideslip and propeller operation on the tail-load distribution. Measurements were also made on the tail-load distribution on the horizontal tail in steady unaccelerated flight over a Mach number range of 0.30 to 0.79 and 0.30 to 0.74, respectively, for the power-on and power-off conditions.
Download or read book Some Flight Measurements of Pressure Distribution During Tail Buffeting written by John Boshar and published by . This book was released on 1945 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of pressure-distribution measurements taken over the horizontal tail surfaces of a Curtiss P-40K airplane during several low-speed pull-ups to abrupt stall in which tail buffeting was experienced.
Download or read book Measurements of the Pressure Distribution on the Horizontal tail Surface of a Typical Propeller driven Pursuit Airplane in Flight written by Melvin Sadoff and published by . This book was released on 1947 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution measurements were made in steady straight and accelerated flight over both sides of the horizontal-tail surface of a typical pursuit airplane up to a Mach number of 0.79. The results showed that a sharply increasing down-load was required to balance the increased diving moment of the wing-fuselage-propeller group at Mach numbers above about 0.70. There was little change, up to a Mach number of about 0.65, of the tail-load gradient (rate of increase of tail load for a unit change in acceleration factor); beyond that Mach number, however, a rapid decrease of tail-load gradient to a Mach number of about 0.73 and then a very sharp increase up to a Mach number of 0.785 was noted. The root bending moments increased considerably on the right tail and decreased, to a lesser extent, on the left tail at the higher Mach numbers, resulting in increased fuselage torsional moments at high speeds. At the higher values of lift coefficient (0.5 to 0.8), there was little change of the lateral distance to the center pressure up to a Mach number of about 0.73; at the highest speed and at low lift coefficients (0 to 0.1) the center of pressure was inboard approximately 3 feet on the left tail and 1.5 feet on the right tail as compared with the values at lower speeds. It appears that satisfactory quantitative data on total tail loads may be obtained from measurements at four stations, equally spaced along the entire tail span.
Download or read book Measurements of the Pressure Distribution on the Horizontal tail Surface of a Typical Propeller driven Pursuit Airplane in Flight written by and published by . This book was released on 1948 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: The total horizontal-tail load and root bending-moment increments calculated by the use of existing rational procedures are compared with the experimental values obtained in abrupt pull-up push-down maneuvers obtained on a representative pursuit-type airplane. The computed loads were determined for the experimental motions and for two estimated linear design motions. The results showed that the actual maximum maneuvering tail loads obtainable in flight could be predicted satisfactorily from either the experimental elevator motions measured in the maneuvers of from the estimated linear elevator motions, provided that good quantitative knowledge was had of pertinent aerodynamic parameters.
Download or read book Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller Driven Pursuit Airplane in Flight 3 Tail Loads in Abrupt Pull Up Push Down Maneuvers written by and published by . This book was released on 1948 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The total horizontal-tail load and the root bending moment increments calculated by the use of existing rational procedures are compared with experimental values obtained in pull-up push-down maneuvers on a representative propeller-driven pursuit-type airplane for six different combinations of power, indicated airspeed, and pressure altitude. The computed loads were determined for the experimental elevator motions, and for two estimated linear design motions. There is also presented a comparison between the computed and the experimental load distributions. Briefly touched upon are two abbreviated static methods for predicting the maximum up-loads in pull-up push-down maneuvers.
Download or read book PRESSURE DISTRIBUTION OF A 0 0667 SCALE MODEL OF THE X 15 AIRPLANE FOR AN ANGLE OF ATTACK RANGE OF 0 DEG TO 28 DEG AT MACH NUMBERS OF 2 30 2 88 AND 4 65 written by and published by . This book was released on 1960 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Pressure Distribution Over the Wings and Tail Surfaces of a PW 9 Pursuit Airplane in Flight written by Richard V. Rhode and published by . This book was released on 1930 with total page 101 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Studies of the Horizontal Tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers Classic Reprint written by Langley Aeronautical Laboratory and published by Forgotten Books. This book was released on 2017-10-28 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Excerpt from Flight Studies of the Horizontal-Tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers It is apparen from the table that the test program progressed from an installation that measured only pres sures on the horizontal tail to one consisting of a combination of pressure orifices and a strain gage and, finally, to an installation which simultaneously measured the pressure, strain, and tail deflection. The strain gage was installed to facilitate an interpretation of the pressure fluctuations experienced on the horizontal tail at and beyond maximum lift of the wing in the pull ups. The apparatus for measuring tail deflection was subsequently added in an effort to obtain additional data on the motion of the tail following the wing stall for correlation with the pressure fluctuations and the strain measurements. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.
