A Flight Investigation Of The Transonic Area Rule For A 525c Sweptback Wind Body Configuration At Mach Numbers Between 08 And 16 PDF Download
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Author | : Sherwood Hoffman |
Publisher | : |
Total Pages | : 30 |
Release | : 1954 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download A Flight Investigation of the Transonic Area Rule for a 52.5© Sweptback Wind-body Configuration at Mach Numbers Between 0.8 and 1.6 Book in PDF, ePub and Kindle
Author | : Sherwood Hoffman |
Publisher | : |
Total Pages | : 24 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download An Investigation of the Transonic Area Rule by Flight Tests of a Sweptback Wing on a Cylindrical Body with and Without Body Indentation Between Mach Numbers 0.9 and 1.8 Book in PDF, ePub and Kindle
Author | : William E. Palmer |
Publisher | : |
Total Pages | : 40 |
Release | : 1956 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Transonic Investigation at Lifting Conditions of Streamline Contouring in the Sweptback-wing-fuselage Juncture in Combination with the Transonic Area Rule Book in PDF, ePub and Kindle
Author | : Robert L. Nelson |
Publisher | : |
Total Pages | : 52 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
Download Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag Book in PDF, ePub and Kindle
Summary: The experimental wave drags of bodies and wing-body combinations over a wide range of Mach numbers are compared with the computed drags utilizing a 24-term Fourier series application of the supersonic area rule and with the results of equivalent-body tests.
Author | : Sherwood Hoffman |
Publisher | : |
Total Pages | : 27 |
Release | : 1958 |
Genre | : |
ISBN | : |
Download Free-flight Investigation at Mach Numbers from 0.8 to 1.5 of the Effect of a Fuselage Indentation on the Zero-lift Drag of a 52.5 Degree Sweptback-wing-body Configuration with Symmetrically Mounted Stores on the Fuselage Book in PDF, ePub and Kindle
Author | : Louis S. Stivers |
Publisher | : |
Total Pages | : 32 |
Release | : 1960 |
Genre | : Airplanes |
ISBN | : |
Download Effects of Fixing Boundary-layer Transition for a Swept- and a Triangular-wing and Body Combination at Mach Numbers from 0.60 to 1.40 Book in PDF, ePub and Kindle
Author | : Lana M. Couch |
Publisher | : |
Total Pages | : 116 |
Release | : 1973 |
Genre | : Aerodynamic load |
ISBN | : |
Download Effect of Blockage Ratio on Drag and Pressure Distributions for Bodies of Revolution at Transonic Speeds Book in PDF, ePub and Kindle
Experimental data were obtained in two wind tunnels for 13 models over a Mach number range from 0.70 to 1.02. Effects of increasing test-section blockage ratio in the transonic region near a Mach number of 1.0 included change in the shape of the drag curves, premature drag creep, delayed drag divergence, and a positive increment of pressures on the model afterbodies. Effects of wall interference were apparent in the data even for a change in blockage ratio from a very low 0.000343 to an even lower 0.000170. Therefore, models having values of blockage ratio of 0.0003 - an order of magnitude below the previously considered safe value of 0.0050 - had significant errors in the drag-coefficient values obtained at speeds near a Mach number of 1.0. Furthermore, the flow relief afforded by slots or perforations in test-section walls - designed according to previously accepted criteria for interference-free subsonic flow - does not appear to be sufficient to avoid significant interference of the walls with the model flow field for Mach numbers very close to 1.0.
Author | : George H. Holdaway |
Publisher | : |
Total Pages | : 58 |
Release | : 1959 |
Genre | : Airplanes |
ISBN | : |
Download Investigation at Mach Numbers of 0.20 to 3.50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave-drag Increase with Increasing Mach Number Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 38 |
Release | : 1960 |
Genre | : |
ISBN | : |
Download Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight Book in PDF, ePub and Kindle
Author | : Michael J. Mann |
Publisher | : |
Total Pages | : 80 |
Release | : 1982 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Supercritical Maneuvering Fighter Configuration Book in PDF, ePub and Kindle