Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
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Brajnikoff, George B↗
Engineering topics
Brajnikoff, George B
Publications and source records attributed to Brajnikoff, George B.
Experimental Investigation of the Effect of Entrance Width-to-height Ratio on the Performance of an Auxiliary Scoop-type Inlet at Mach Numbers from 0 to 1.3
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Brajnikoff, George B↗
Method and graphs for the evaluation of air-induction systems
Graphs have been developed for rapid evaluation of air-induction systems from considerations of their aerodynamic-performance parameters in combination with power-plant characteristics. The graphs cover the range of supersonic Mach numbers to 3.0. Examples are presented for an air-induction system and engine combination of two Mach numbers and two altitudes in order to illustrate the method and application of the graphs. The examples show that jet-engine characteristics impose restrictions on the use of fixed inlets if the maximum net thrusts are to be realized at all flight conditions. (author)
Brajnikoff, George B↗
Method and Graphs for the Evaluation of Air-induction Systems
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Brajnikoff, George B↗
Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0.
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Brajnikoff, George B↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area IV : Some Effects of Internal Duct Shape upon an Inlet Enclosing 37.2 Percent of the Forebody Circumference
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Davis, Wallace F↗
An Experimental Investigation at Supersonic Speeds of Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer
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Davis, Wallace F↗
Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer II : Effect of an Oblique Shock Wave Immediately Ahead of the Inlet
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Brajnikoff, George B↗
Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer I : Addition of Energy to the Boundary Layer
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Davis, Wallace F↗