Numerical investigation on the aerodynamic efficiency of bio-inspired corrugated and cambered airfoils in ground effect. [PDF]
Abdizadeh GR +2 more
europepmc +1 more source
Aeronautical engineering: A continuing bibliography, supplement 122 [PDF]
This bibliography lists 303 reports, articles, and other documents introduced into the NASA scientific and technical information system in April ...
core +1 more source
Fiber-optic integrated aerodynamic three-hole vector probe for high-velocity flow field measurement. [PDF]
Liu Y +9 more
europepmc +1 more source
The aerodynamic challenges of the design and development of the space shuttle orbiter [PDF]
The major aerodynamic design challenge at the beginning of the United States Space Transportation System (STS) research and development phase was to design a vehicle that would fly as a spacecraft during early entry and as an aircraft during the final ...
Gamble, J. D. +9 more
core +1 more source
Aeronautical Engineering: A special bibliography with indexes, supplement 74 [PDF]
This special bibliography lists 295 reports, articles, and other documents introduced into the NASA scientific and technical information system in August ...
core +1 more source
A reinforcement learning approach to airfoil shape optimization. [PDF]
Dussauge TP +3 more
europepmc +1 more source
Solution of transonic flows by an integro-differential equation method [PDF]
Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integro-differential equation which involves a tangential derivative of the perturbation velocity potential.
Ogana, W.
core +1 more source
Applied aerodynamics: Challenges and expectations [PDF]
Aerospace is the leading positive contributor to this country's balance of trade, derived largely from the sale of U.S. commercial aircraft around the world.
Peterson, Victor L., Smith, Charles A.
core +1 more source
Skin-Friction-Based Identification of the Critical Lines in a Transonic, High Reynolds Number Flow via Temperature-Sensitive Paint. [PDF]
Costantini M +3 more
europepmc +1 more source
Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing [PDF]
The flow over the B-1 wing is studied computationally, including the aeroelastic response of the wing. Computed results are compared with results from wind tunnel and flight tests for both low-sweep and high-sweep cases, at 25.0 deg.
Goorjian, P. M. +3 more
core +1 more source

