Experimental ablation cooling
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Bond, Aleck C↗
Engineering topics
Bond, Aleck C
Publications and source records attributed to Bond, Aleck C.
Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07
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O'Neal, Robert L↗
Free-flight Skin-temperature and Surface-pressure Measurements on a Highly Polished Nose Having a 100 Degree Total-angle Cone and a 10 Degree Half-angle Conical Flare Section up to a Mach Number of 4.08
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Rashis, Bernard↗
Aerodynamic heat transfer to wing surfaces and wing leading edges
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Bond, Aleck C↗
Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 degree delta-wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70
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Bond, Aleck C↗
Experimental Investigation of a Flat Plate Paddle Jet Vane Operating on a Rocket Jet
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Bond, Aleck C↗