Results 131 to 140 of about 31,952 (223)

Jet aircraft emissions during cruise: Present and future [PDF]

Forecasts of engine exhaust emissions that may be practicably achievable for future commercial aircraft operating at high altitude cruise conditions are compared to cruise emission for present day aircraft.
Grobman, J. S.
core   +1 more source

Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft, volume 1 [PDF]

This bibliography was developed as a first step in the preparation of a monograph on the subject of the aerodynamics of airframe/engine integration of high speed turbine powered aircraft.
Nichols, M. R.
core   +1 more source

A methodology for designing aircraft to low sonic boom constraints [PDF]

A method for designing conceptual supersonic cruise aircraft to meet low sonic boom requirements is outlined and described. The aircraft design is guided through a systematic evolution from initial three view drawing to a final numerical model ...
Mack, Robert J., Needleman, Kathy E.
core   +1 more source

Aerodynamic Testing of a 3D-Printed Aircraft Model with a Post-Processed Surface. [PDF]

Materials (Basel)
Setlak L, Kowalik R, Lusiak T.
europepmc   +1 more source

Complementary Design of Two Types of Signals for Avionic Phased-MIMO Weather Radar. [PDF]

Sensors (Basel)
Geng Z, Wang L, Meng F, Wu D, Zhu D.
europepmc   +1 more source

Contracts, grants and funding summary of supersonic cruise research and variable-cycle engine technology programs, 1972 - 1982 [PDF]

NASA-SCAR (AST) program was initiated in 1972 at the direct request of the Executive Office of the White House and Congress following termination of the U.S. SST program.
Hoffman, S., Varholic, M. C.
core   +1 more source

High-Reynolds-Number Turbulence Database: AeroFlowData. [PDF]

Sci Data
Zhang W, Shan X, Liu Y, Zhang X, Wan Z, Li X, Sha X, Zhao J, Xu H, He C, Liu Y, Xia Z, Li W, Gao L, Jin X, Li H, Liao F, Zhang Y, Chen G.   +18 more
europepmc   +1 more source

Numerical simulation of ellipse liquid jet atomization in supersonic crossflow. [PDF]

Sci Rep
Zhou D, Li Y, Chang J.
europepmc   +1 more source

Study of active cooling for supersonic transports [PDF]

The potential benefits of using the fuel heat sink of hydrogen fueled supersonic transports for cooling large portions of the aircraft wing and fuselage are examined.
Brewer, G. D., Morris, R. E.
core   +1 more source

Research progress on aero-optical effects of hypersonic optical window with film cooling. [PDF]

Light Sci Appl
Yi S, Ding H, Luo S, Sun X, Xia Z.
europepmc   +1 more source