An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds
| Title | An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF eBook |
| Author | Charles F. Whitcomb |
| Publisher | |
| Pages | 286 |
| Release | 1961 |
| Genre | |
| ISBN |
Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
| Title | Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body PDF eBook |
| Author | Donald D. Arabian |
| Publisher | |
| Pages | 88 |
| Release | 1960 |
| Genre | Aerodynamics, Transonic |
| ISBN |
The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
Loads on Thin Wings at Transonic Speeds
| Title | Loads on Thin Wings at Transonic Speeds PDF eBook |
| Author | Don D. Davis (Jr.) |
| Publisher | |
| Pages | 22 |
| Release | 1955 |
| Genre | Aerodynamics, Transonic |
| ISBN |
A 1-foot Hypervelocity Shock Tunnel in which High-enthalpy, Real-gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds
| Title | A 1-foot Hypervelocity Shock Tunnel in which High-enthalpy, Real-gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds PDF eBook |
| Author | Bernard E. Cunningham |
| Publisher | |
| Pages | 48 |
| Release | 1962 |
| Genre | Aerodynamics |
| ISBN |
Apollo Program Summary Report
| Title | Apollo Program Summary Report PDF eBook |
| Author | |
| Publisher | |
| Pages | 526 |
| Release | 1975 |
| Genre | |
| ISBN |
The Apollo Spacecraft: Ertel, I. D. and Morse, M. L. Through November 7, 1962
| Title | The Apollo Spacecraft: Ertel, I. D. and Morse, M. L. Through November 7, 1962 PDF eBook |
| Author | Ivan D. Ertel |
| Publisher | |
| Pages | 292 |
| Release | 1969 |
| Genre | Government publications |
| ISBN |
An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel
| Title | An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel PDF eBook |
| Author | Ralph P. Bielat |
| Publisher | |
| Pages | 44 |
| Release | 1951 |
| Genre | Aerodynamics, Transonic |
| ISBN |
Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.