A Study of Stall Phenomena on a 45 Degree Swept-forward Wing
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AIRFOILS - NACA 64A112 (A=0 8)(MOD ) - CHAR & ORDI↗
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Results for “phenomena”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Method for evaluating from shadow or Schlieren photographs the pressure drag in two-dimensional or axially symmetrical flow phenomena with detached shock
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SHADOW METHOD↗
The design, operation, and uses of the water channel as an instrument for the investigation of compressible-flow phenomena
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WATER TUNNELS - NACA (AMER )↗
A New Shadowgraph Technique for the Observation of Conical Flow Phenomena in Supersonic Flow and Preliminary Results Obtained for a Triangular Wing
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Love, Eugene S↗
A Low-density Wind-tunnel Study of Shock-wave Structure and Relaxation Phenomena in Gases
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Sherman, F S↗
An Investigation of Some Phenomena Relating to Aural Detection of Airplanes
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Hubbard, Harvey H↗
Investigation at large scale of the pressure distribution and flow phenomena over a wing with the leading edge swept back 47.5 degrees having circular-arc airfoil sections and equipped with drooped-nose and plain flaps
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Lange, Roy H↗
Observations of Unsteady Flow Phenomena for an Inclined Body Fitted with Stabilizing Fins
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Mead, Merrill H↗
The calculation of certain static aeroelastic phenomena of wings with tip tanks or boom-mounted lifting surfaces
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Diederich, Franklin W↗
Visualization of secondary-flow phenomena in blade row
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Herzig, H Z↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination
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Robinson, Harold L↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination
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Williams, Claude V↗
Static aeroelastic phenomena of M-, W-, and A-wings
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Diederich, Franklin W↗
An Experimental Investigation of the Flow Phenomena over Bodies at High Angles of Attack at a Mach Number of 2.01
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Gapcynski, John P↗
Preliminary Survey of Compressor Rotor-blade Wakes and Other Flow Phenomena with a Hot-wire Anemometer
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Fessler, Theodore E↗
Some Reynolds Number Phenomena in a Turbojet Compressor
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Kaufman, Harold R↗
Ignition and combustion phenomena in Diesel engines
Evidences were found that neither gasification nor vaporization of the injected fuel occurs before ignition; also that the hydrogen coefficient has no significance. However the knowledge of the ignition point and of the "time lag" is important. After ignition, the combustion proceeds in a series of reactions, the last of which at least are now known.
ENGINES, DIESEL - IGNITION & COMBUSTION↗
Observations of Compressibility Phenomena in Flight
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AIRPLANES - BREWSTER F2A-2 FLIGHT TESTS (AMER )↗