Results 51 to 60 of about 10,858 (135)

Aeronautical engineering: A continuing bibliography, supplement 122 [PDF]

open access: yes
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]

open access: yesiScience, 2022
Liu Y   +9 more
europepmc   +1 more source

The aerodynamic challenges of the design and development of the space shuttle orbiter [PDF]

open access: yes
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]

open access: yes
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]

open access: yesSci Rep, 2023
Dussauge TP   +3 more
europepmc   +1 more source

Solution of transonic flows by an integro-differential equation method [PDF]

open access: yes
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]

open access: yes
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

Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing [PDF]

open access: yes
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

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