Load distributions associated with controls at supersonic speeds
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Czarnecki, K R↗
Engineering topics
Lord, Douglas R
Publications and source records attributed to Lord, Douglas R.
Hinge-moment Characteristics for Several Tip Controls on a 60 Degree Sweptback Delta Wing at Mach Number 1.61
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Czarnecki, K R↗
Pressure Measurements on an Ogive-cylinder Body at Mach Number 4.04
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Lord, Douglas R↗
An Investigation of Flow Characteristics at Mach Number 4.04 over 6- and 9-percent-thick Symmetrical Circular-arc Airfoils Having 30-percent-chord Trailing-edge Flaps
Section data obtained from wind-tunnel tests at Mach number 4.04 and Reynolds numbers of about 5.0 times 10 to the 6th power and 8.4 times 10 to the 6th power are presented for 6- and 9-percent-thick symmetrical circular-arc airfoils with 30 percent chord trailing-edge flaps. Pressure distributions, Schlieren photographs, and force and moment coefficients are included.
FLOW, VISCOUS↗
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds
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Daley, Bernard N↗