Lateral Motions Encountered with the Douglas D-558-II All-rocket Research Airplane During Exploratory Flights to a Mach Number of 2.0
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Ankenbruck, Herman O↗
Engineering topics
Ankenbruck, Herman O
Publications and source records attributed to Ankenbruck, Herman O.
Determination of longitudinal handling qualities of the D-558-II research airplane at transonic and supersonic speeds to a Mach number of about 2.0
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Ankenbruck, Herman O↗
Determination of Longitudinal Stability in Supersonic Accelerated Maneuvers for the Douglas D-558-II Research Airplane
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Ankenbruck, Herman O↗
Some Measurements of Flying Qualities of a Douglas D-558-II Research Airplane During Flights to Supersonic Speeds
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Ankenbruck, Herman O↗
Stability and Control Measurements Obtained During USAF-NACA Cooperative Flight-test Program on the X-4 Airplane (USAF No. 46-677)
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Ankenbruck, Herman O↗
Generalized Performance Comparison of Large Conventional, Tail Boom, and Tailless Airplanes
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AIRPLANES, TAILLESS↗
Effects of Tip Dihedral on Lateral Stability and Control Characteristics as Determined by Tests of a Dynamic Wind Model in the Langley Free-flight Tunnel
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Ankenbruck, Herman O↗
Determination of the Stability and Control Characteristics of a Straight-Wing, Tailless Fighter-Airplane Model in the Langley Free-Flight Tunnel
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CENTER OF GRAVITY - POSITION↗
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
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STABILITY, LONGITUDINAL - POWER-OFF↗
Maximum lift coefficients of airplanes based on sum of wing and tail areas
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TAIL SURFACES - AREA↗