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United States.: National Advisory Committee for Aeronautics | Akateeminen Kirjakauppa

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PROBLEM OF SLIP FLOW IN AERODYNAMICS

United States.: National Advisory Committee for Aeronautics
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CALCULATION OF THE SHAPE OF A TWO-DIMENSIONAL SUPERSONIC NOZZLE IN CLOSED FORM

United States.: National Advisory Committee for Aeronautics
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15,30 €

ON THE THREE-DIMENSIONAL INSTABILITY OF LAMINAR BOUNDARY LAYERS ON CONCAVE WALLS

United States.: National Advisory Committee for Aeronautics
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15,30 €

AIRFOIL MEASUREMENTS IN THE DVL HIGH-SPEED WIND TUNNEL (2.7-METER DIAMETER) : = PROFILMESSUNGEN IM DVL-HOCHGESCHWINDIGKEITSWINDK

United States.: National Advisory Committee for Aeronautics
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15,30 €

GAS MOTION IN A LOCAL SUPERSONIC REGION AND CONDITIONS OF POTENTIAL-FLOW BREAKDOWN

United States.: National Advisory Committee for Aeronautics
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RESISTANCE OF CASCADE OF AIRFOILS IN GAS STREAM AT SUBSONIC VELOCITY

United States.: National Advisory Committee for Aeronautics
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FORMATION OF A VORTEX AT THE EDGE OF A PLATE

United States.: National Advisory Committee for Aeronautics
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ON THE SPECTRUM OF NATURAL OSCILLATIONS OF TWO-DIMENSIONAL LAMINAR FLOWS

United States.: National Advisory Committee for Aeronautics
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ON THE STATISTICAL THEORY OF TURBULENCE

United States.: National Advisory Committee for Aeronautics
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CONCERNING THE FLOW ABOUT RING-SHAPED COWLINGS.: PART II, ANNULAR BODIES OF INFINITE LENGTH WITH CIRCULATION FOR SMOOTH ENTRANCE

United States.: National Advisory Committee for Aeronautics
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15,40 €

PLANE PROBLEM OF THE FLAPPING WING

United States.: National Advisory Committee for Aeronautics
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15,40 €

AMPLITUDE DISTRIBUTION AND ENERGY BALANCE OF SMALL DISTURBANCES IN PLATE FLOW : = AMPLITUDENVERTEILUNG UND ENERGIEBILANZ DER KLE

United States.: National Advisory Committee for Aeronautics
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15,40 €

LAMINAR FLOW ABOUT A ROTATING BODY OF REVOLUTION IN AN AXIAL AIRSTREAM

United States.: National Advisory Committee for Aeronautics
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15,40 €

ON THE TURBULENT FRICTION LAYER FOR RISING PRESSURE

United States.: National Advisory Committee for Aeronautics
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15,40 €

DISPLACEMENT EFFECT OF THE LAMINAR BOUNDARY LAYER AND THE PRESSURE DRAG

United States.: National Advisory Committee for Aeronautics
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INVESTIGATIONS OF THE BOUNDARY-LAYER CONTROL ON A FULL SCALE SWEPT WING WITH AIR BLED OFF FROM THE TURBOJET

United States.: National Advisory Committee for Aeronautics
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15,40 €

KINETIC TREATMENT OF THE NUCLEATION IN SUPERSATURATED VAPORS

United States.: National Advisory Committee for Aeronautics
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15,40 €

HEAT TRANSMISSION IN THE BOUNDARY LAYER

United States.: National Advisory Committee for Aeronautics
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15,40 €

FLAT WING WITH SHARP EDGES IN A SUPERSONIC STREAM

United States.: National Advisory Committee for Aeronautics
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15,40 €

ELLIPTIC WING BASED ON THE POTENTIAL THEORY

United States.: National Advisory Committee for Aeronautics
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15,40 €

Hae lisää...

Problem of slip flow in aerodynamics

United States.: National Advisory Committee for Aeronautics

15,30 €

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Kieli: Venäjä

Vosproizvedeno v original'noj avtorskoj orfografii izdaniya 1957 goda (izdatel'stvo "Washington, D.C. : National Advisory Committee for Aeronautics").

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ISBN:

9785882123108

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