Additional experiments with flat-top wing-body combinations at high supersonic speeds
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Syvertson, Clarence A↗
Engineering topics
Wong, Thomas J
Publications and source records attributed to Wong, Thomas J.
A preliminary investigation of the static stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
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Wong, Thomas J↗
Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28
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Savin, Raymond C↗
Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 and 5.05
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Gloria, Hermilo R↗
Aerodynamic characteristics of two rectangular-plan-form, all moveable controls in combination with a slender body of revolution at Mach numbers from 3.00 to 6.25
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Wong, Thomas J↗
Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
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Neice, Stanford E↗
An Experimental Investigation of the Applicability of the Hypersonic Similarity Law to Bodies of Revolution
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Neice, Stanford E↗
The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight
The similarity law for nonsteady, inviscid, hypersonic flow about slender three-dimensional shapes is derived. Conclusions drawn are shown to be valid for rotational flow. Requirements for dynamic similarity of related shapes in free flight are obtained. The law is examined for steady flow about related three-dimensional shapes. Results of an experimental investigation of the pressures acting on two inclined cones are found to check the law as it applies to bodies of revolution.
Hamaker, Frank M↗
The similarity law for nonsteady hypersonic flows and requirements for the dynamical similarity of related bodies in free flight
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Hamaker, Frank M↗