Obara et al., 1985 - Google Patents
Flight-measured laminar boundary-layer transition phenomena including stability theory analysisObara et al., 1985
View PDF- Document ID
- 3259629015062599345
- Author
- Obara C
- Holmes B
- Publication year
External Links
Snippet
Flight experiments were conducted on a single-engine turboprop aircraft fitted with a 92-in- chord, 3-ft-span natural laminar flow glove at glove section lift coefficients from 0.15 to 1.10. The boundary-layer transition measurement methods used included sublimating chemicals …
- 238000004458 analytical method 0 title abstract description 21
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/10—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring thermal variables
- G01P5/12—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring thermal variables using variation of resistance of a heated conductor
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
- G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P13/00—Indicating or recording presence, absence, or direction, of movement
- G01P13/02—Indicating direction only, e.g. by weather vane
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Obara et al. | Flight-measured laminar boundary-layer transition phenomena including stability theory analysis | |
| Poll | Transition in the infinite swept attachment line boundary layer | |
| Horstmann et al. | Flight tests with a natural laminar flow glove on a transport aircraft | |
| Addy, Jr et al. | A wind tunnel study of icing effects on a natural laminar flow airfoil | |
| Eckstrom et al. | Measurements of unsteady pressure and structural response for an elastic supercritical wing | |
| Marchman III et al. | Aerodynamics of an aspect ratio 8 wing at low Reynolds numbers | |
| Smith et al. | Measurement of the speed of sound in ice | |
| Chapman et al. | Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw | |
| Mabey | An hypothesis for the prediction of flight penetration of wing buffeting from dynamic tests on wind tunnel models | |
| Newton et al. | Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil: Flight test data | |
| Van Dam et al. | Leading-edge transition and relaminarization phenomena on a subsonichigh-lift system | |
| Wentz Jr et al. | Further results of natural laminar flow flight test experiments | |
| Kemmerly et al. | Investigation of a moving-model technique for measuring ground effect | |
| Davison et al. | NRC Particle Detection Probe: Results and Analysis from Ground and Flight Tests | |
| Chiles et al. | Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection on high-performance aircraft | |
| Anderson et al. | Techniques used in the F-14 variable-sweep transition flight experiment | |
| Heldenfels et al. | Test of an Aerodynamically Heated Multiweb Wing Structure (MW-1) in a Free Jet at Mach Number 2 | |
| Holmes et al. | Flight research on natural laminar flow applications | |
| Butler et al. | Wind-Tunnel/Flight Comparison of the Levels of Buffeting Response Intensity for the TACT F-111. | |
| Holmes | Flight experiences with laminar flow | |
| Rivers | Flight investigation of the effects of pressure-belt tubing size on measured pressure distributions | |
| Saiki | Effects of an aft facing step on the surface of a laminar flow glider wing | |
| Muhlstein Jr et al. | Integration time required to extract accurate data from transonic wind-tunnel tests | |
| Otten et al. | Atmospheric turbulence measurements from a subsonic aircraft | |
| Ahmed et al. | In-flight boundary-layer transition measurements on a swept wing |