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Herman O Ankenbruck

Observed names: Ankenbruck, H. O., Ankenbruck, Herman O, Ankenbruck, Herman O., H. ANKENBRUCK, HERMAN O. ANKENBRUCK
Observed institution: Bendix (United States)
OpenAlex ID: A5023536258
Generalized performance comparison of large conventional, tail boom, and tailless airplanes
1947 · Herman O Ankenbruck, Marion O Mckinney · 2
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
1945 · Herman O Ankenbruck · NASA STI Repository (National Aeronautics and Space Administration) · 1
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An approach to penetration cost effectiveness evaluation.
1967 · HERMAN O. ANKENBRUCK · Journal of Aircraft
An approach to penetration cost effectiveness evaluation
1966 · H. ANKENBRUCK
Lateral Motions Encountered with the Douglas D-558-II All-Rocket Research Airplane During Exploratory Flights to a Mach Number of 2.0
1954 · Herman O Ankenbruck, C. H. Wolowicz · NASA STI Repository (National Aeronautics and Space Administration)
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
1954 · Herman O Ankenbruck · NASA Technical Reports Server (NASA)
Determination of longitudinal stability in supersonic accelerated maneuvers for the Douglas D-558-II research airplane
1954 · Herman O Ankenbruck · NASA STI Repository (National Aeronautics and Space Administration)
Some Measurements of Flying Qualities of a Douglas D-558-II Research Airplane During Flights to Supersonic Speeds
1953 · Herman O Ankenbruck, Theodore E Dahlen · NASA STI Repository (National Aeronautics and Space Administration)
NACA Research Memorandums
1953 · Ankenbruck, Herman O., Dahlen, Theodore E. · University of North Texas Digital Library (University of North Texas)
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Stability and Control Measurements Obtained During USAF-NACA Cooperative Flight-test Program on the X-4 Airplane (USAF No. 46-677)
1951 · Herman O Ankenbruck, Melvin Sadoff, et al. · NASA Technical Reports Server (NASA)
An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot
1950 · Robert A. Gardiner, Jacob Zarovsky, et al. · NASA Technical Reports Server (NASA)
Estimation of range of stability derivatives for current and future pilotless aircraft
1947 · Marvin Pitkin, Herman O Ankenbruck
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
1946 · Herman O Ankenbruck · NASA STI Repository (National Aeronautics and Space Administration)
NACA Technical Notes
1946 · Ankenbruck, Herman O., McKinney, Marion O., Jr. · University of North Texas Digital Library (University of North Texas)
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Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel
1946 · Herman O Ankenbruck · NASA STI Repository (National Aeronautics and Space Administration)
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NACA Advanced Confidential Reports
1945 · Seacord, Charles L., Jr., Ankenbruck, Herman O. · University of North Texas Digital Library (University of North Texas)
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Maximum lift coefficients of airplanes based on sum of wing and tail areas
1944 · Herman O Ankenbruck · NASA Technical Reports Server (NASA)
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NACA Restricted Bulletins
1944 · Ankenbruck, Herman O. · University of North Texas Digital Library (University of North Texas)
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Works count: 23
Citation count: 3
H-index: 1
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