Robert H. Liebeck
American aerospace engineer
Robert H. Liebeck's AcademicInfluence.com Rankings
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Engineering
Robert H. Liebeck's Degrees
- Masters Aerospace Engineering Stanford University
- PhD Aerospace Engineering Stanford University
Why Is Robert H. Liebeck Influential?
(Suggest an Edit or Addition)According to Wikipedia, Robert Hauschild Liebeck is an American aerodynamicist, professor and aerospace engineer. Until retiring from his position as senior fellow at the Boeing Company. in 2020, he oversaw their Blended Wing Body program. He has been a member of the National Academy of Engineering since 1992, where he is an AIAA Honorary Fellow, the organization’s highest distinction. He is best known for his contributions to aircraft design and his pioneering airfoil designs known as the "Liebeck Airfoil". Since his retirement he remains active in aviation industry associations and continues to teach at UCI.
Robert H. Liebeck's Published Works
Published Works
- Design of the Blended Wing Body Subsonic Transport (2002) (621)
- Design of Subsonic Airfoils for High Lift (1978) (538)
- Design of optimum propellers (1983) (225)
- BLENDED-WING-BODY SUBSONIC COMMERCIAL TRANSPORT (1998) (202)
- Modeling and Computation of Boundary-Layer Flows (1998) (177)
- Design of the Blended-Wing-Body subsonic transport (2002) (175)
- A Class of Airfoils Designed for High Lift in Incompressible Flow (1973) (135)
- Vortex generators used to control laminar separation bubbles (1990) (98)
- Blended Wing Body analysis and design (1997) (79)
- Advanced Subsonic Airplane Design and Economic Studies (1995) (74)
- Optimization of airfoils for maximum lift (1969) (72)
- An experimental investigation of boundary layer ingestion in a diffusing S-duct with and without passive flow control (1999) (68)
- AERODYNAMIC DESIGN CHALLENGES OF THE BLENDED-WING-BODY SUBSONIC TRANSPORT (2000) (65)
- N+3 Aircraft Concept Designs and Trade Studies. Volume 2; Appendices-Design Methodologies for Aerodynamics, Structures, Weight, and Thermodynamic Cycles (2010) (59)
- N+3 Aircraft Concept Designs and Trade Studies. Volume 1 (2010) (46)
- BLENDED WING BODY DESIGN CHALLENGES (2003) (34)
- A Comparison Between Boundary Layer Measurements in a Laminar Separation Bubble Flow and Linear Stability Theory Calculations (1989) (31)
- Laminar separation bubbles and airfoil design at low Reynolds numbers (1992) (30)
- Some Thoughts on the Design of Subsonic Transport Aircraft for the 21st Century (1990) (26)
- Multidisciplinary optimization on an advanced composite wing (1996) (25)
- An experimental study of vortex generators in boundary layer ingesting diffusers with a centerline offset (1999) (20)
- Experimental Investigation of Boundary Layer Ingesting Diffusers of a Semi-Circular Cross Section (1998) (18)
- An experimental study of the effect of offset on thick boundary layers flowing inside diffusing ducts (1999) (15)
- Study of Slat-Airfoil Combinations Using Computer Graphics (1973) (14)
- On the design of subsonic airfoils for high lift (1976) (13)
- Evolution of the revolutionary blended-wing-body (1996) (13)
- Low Reynolds Number Airfoil Design for Subsonic Compressible Flow (1989) (10)
- Calculation of low Reynolds number flows at high angles of attack (1990) (7)
- Three-dimensional calculation of windmill surface pressures (1988) (3)
- A Simple Model for the Theoretical Study of Slat-Airfoil Combinations, (1972) (3)
- Low Reynolds Number - Separation Bubble (1987) (3)
- Theoretical Studies on the Aerodynamics of Slat-Airfoil Combinations (1971) (2)
- Charts and Formulas for Estimating Velocity Fields in Incompressible Flow (1968) (2)
- Analysis and design of dual-rotation propellers (1989) (2)
- Multiple Application Propfan Study (MAPS): Advanced tactical transport (1986) (1)
- Design and Flight Testing of a Multirotor Vehicle with Cyclic-Collective Pitch Control (2020) (1)
- Flight Test of the Blended Wing Body X-48B (2008) (0)
- One-Dimensional Flow Properties for a Specified Dissociation Variation of an Inviscid Diatomic Gas (1962) (0)
- 16.885J / ESD.35J Aircraft Systems Engineering, Fall 2003 (2003) (0)
- The vortex-blade element propeller design and analysis pro- Q = torque cedure defined by Adkins and Liebeck has been extended to the design and analysis of counterrotating propellers. The (1989) (0)
- Book Reviews: Airfoil Design and Data- Richard Eppler (1993) (0)
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What Schools Are Affiliated With Robert H. Liebeck?
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