Research memoranda / National Advisory Committee for Aeronautics, NACA

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Bibliographische Detailangaben
Körperschaft: USA National Advisory Committee for Aeronautics (VerfasserIn)
Format: UnknownFormat
Veröffentlicht: Washington, DC 1946-
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Titel Jahr Band
Experimental shock configurations and shock losses in a transonic-compressor rotor at design speed 1958
Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20 1958
Comparison of performance of two aerodynamically similar 14-inch-diameter single-stage compressor rotors of different chord length 1958
Limited investigation of noise suppression by injection of water into exhaust of afterburning jet engine 1958
Effectiveness of various protective coverings on magnesium fins at Mach number 2.0 and stagnation temperatures up to 3,600 R 1958
Investigation of effects of Reynolds number on over-all performance of an eight-stage axial-flow research compressor with two transonic inlet stages 1957
Exploration investigation of static- and base-pressure increases resulting from combustion of aluminum borohydride adjacent to body of revolution in supersonic wind tunnel 1957
A balanced-pressure sliding seal for transfer of pressurized air between stationary and rotating parts 1957
Investigation of a high-performance axial-flow compressor transonic inlet rotor designed for 37.5 pounds per second per square foor of frontal area : detailed blade-element performance 1957
Measurements of heat transfer and boundary-layer transition on an 8-inch-diameter hemisphere-cylinder in free flight for a Mach number range of 2.00 to 3.88 1957
Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance 1957
Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94 1957
Exploratory investigation of aerodynamic effects of external combustion of aluminum borohydride in airstream adjacent to flat plate in mach 2.46 tunnel 1957
A transonic investigation of the mass-flow and pressure recovery characteristics of several types of auxiliary air inlets 1957
Internal performance of several auxiliary air inlets immersed in a turbulent boundary layer at Mach numbers of 1.3, 1.5, and 2.0 1957
Statistical approach to the estimation of loads and pressures on seaplane hulls for routine operations 1957
A study of symmetrical, circular, internal compression inlet 1956
Altitude performance of J71-A-2(600-D1) turbojet engine 1956
Tables and charts for thermodynamic calculations involving air and fuels containing boron, carbon, hydrogen, and oxygen 1956
Influence of new boric-oxide vapor-pressure data on calculated performance of pentaborane 1956
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