Foote, 1959 - Google Patents
Sigurd HoyerFoote, 1959
View HTML- Document ID
- 14126462902071794025
- Author
- Foote J
- Publication year
- Publication venue
- Studies on Dynamics and Instrumentation of the Holloman Track
External Links
Snippet
The aerodynamic lift on a supersonic sled is studied and traced to a variety of causes. For an existing sled operating at Mach numbers up to 1.5 a qualitative analysis shows some faults which should have been avoided. For sleds in general the problems investigated include …
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water data:image/svg+xml;base64,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 data:image/svg+xml;base64,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 O 0 abstract description 15
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2724966A (en) | High speed landcraft | |
| CN112067232B (en) | A hypersonic wind tunnel test system and method for simulating the ground effect of a rocket sled | |
| CN106932187B (en) | Device and method for testing protruding of nose landing gear of carrier-based aircraft | |
| US3152775A (en) | Supersonic aircraft | |
| CN107677446A (en) | A kind of water surface flying device hydrodynamic(al) method for testing performance under heel state | |
| Foote | Sigurd Hoyer | |
| Xia et al. | Research on a new open water-brake method for double-track rocket sled test | |
| Dathe et al. | Hydrodynamic characteristics of seaplanes as affected by hull shape parameters | |
| CN115950315B (en) | A double-track rocket sled aerodynamic shape structure suitable for hypersonic speed | |
| Mat | The analysis of flow on round-edged delta wings | |
| WOHLLEBE et al. | Some basic test results of V/STOL jet induced lift effects in hover | |
| RU223804U1 (en) | Airplane with emergency landing flaps | |
| Kenyon | A Preliminary Investigation of Modified Blunt 13 Half-Cone Re-Entry Configurations at Subsonic Speeds | |
| Boddy | Investigation at High Subsonic Speeds of Methods of Alleviating the Adverse Interference at the Root of a Swept-Back Wing | |
| WOOD et al. | The control of vortical flow on a delta wing at high angles of attack | |
| Torda et al. | Aerodynamic design of a Land Speed Record car | |
| Davidson et al. | Some Systematic Model Experiments on the Porpoising Characteristics of Flying-Boat Hulls | |
| MARCHMAN, III et al. | Performance improvement of delta wings at subsonic speeds due to vortex flaps | |
| Lee et al. | Active Control of Forebody Vortices on a Schematic Aircraft Model | |
| Guy | Loads on External Stores at Transonic and Supersonic Speeds | |
| Kaplan | On a new method for calculating the potential flow past a body of revolution | |
| Alford Jr | Effects of wing-fuselage flow fields on missile loads at subsonic speeds | |
| Dowty | Aircraft Alighting and Arresting Mechanisms | |
| Benson et al. | The Effect of Dead Rise upon the High-Angle Porpoising Characteristics of Two Planing Surfaces in Tandem | |
| Winston et al. | Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large-scale Six-propeller VTOL Model at Static Thrust: Matthew M. Winston and Robert J. Huston |