Results 171 to 180 of about 33,063 (224)

Analysis of the Environmental Impact of Currently Developed Supersonic Civil Aircraft Engines

Russian Engineering Research
S. S. Ogorodnikov, S. V. Ogorodnikova
openaire   +2 more sources

The impact of design space constraints on the noise and emissions from derivative engines for civil supersonic aircraft

AIAA Scitech 2021 Forum, 2021
Laurens Voet, Prakash Prashanth, Raymond Speth, Jayant Sabnis, Choon Tan, Steven Barrett   +5 more
openaire   +2 more sources

The Case for Small Supersonic Civil Aircraft

AIAA International Air and Space Symposium and Exposition: The Next 100 Years, 2003
P. Henne
openaire   +2 more sources

Numerical studies of nozzle thrust characteristics of supersonic civil aircraft by computational gas dynamics method

Vestnik Moskovskogo aviatsionnogo instituta, 2019
Vladlen Gorbovskoi, Andrey Kazhan, Vyacheslav Kazhan, Andre Shenkin   +3 more
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A FLAT JET NOZZLE INTEGRATION WITH THE SUPERSONIC CIVIL AIRCRAFT PLANE WITH A LOW LEVEL OF SONIC BOOM

22-st INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2022)
A.V. Shenkin, A.A. Saveliev, I.S. Matyash, G.N. Lavrukhin, V.S. Gorbovskoy, A.V. Lysenkov   +5 more
openaire   +2 more sources

Preliminary Optimization of the Sonic Boom Properties for Civil Supersonic Aircraft

Journal of Aircraft, 2013
In this work a simple model has been used that relates sonic boom effects to the main geometric and operative parameters of the civil supersonic aircraft. In particular, a relation between the maximum overpressure and the aircraft shape factor is employed to define an optimal preliminary design point for the supersonic civil aircraft.
SCARSELLI, Gennaro, E. Castorini
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Engines for Supersonic Civil Transport Aircraft

Aircraft Engineering and Aerospace Technology, 1961
Because of its high overall pressure ratio and good propulsive efficiency, the jet engine is very efficient for supersonic propulsion. A high thrust per unit power plant frontal area and per unit weight are primary requirements and these imply high combustion temperatures. For a Mach 2.0 aircraft, engine design problems other than this are not outside
openaire   +1 more source

COMPUTATIONAL AND EXPERIMENTAL STUDIES OF THE NEAR FIELD OF THE SUPERSONIC CIVIL AIRCRAFT MODEL IN THE WT T-112

22-st INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2022)
D.S. Sboev, V.N. Radchenko, V.E. Mosharov, S.I. Konovalov, A.V. Zabrodin, V.S. Gorbovskoy, G.V. Biryukov, S.A. Baranov, S.N. Tolkachev   +8 more
openaire   +2 more sources

Real-time obstacle detection system for high speed civil transport supersonic aircraft

Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093), 2002
The High Speed Civil Transport (HSCT) supersonic commercial aircraft under development by National Aeronautics and Space Administration (NASA) and its partners is expected to include an eXternal Visibility System (XVS) to aid the pilot's limited view through their cockpit windows.
null Mau-Tsuen Yang, T. Gandhi, R. Kasturi, L. Coraor, O. Camps, J. McCandless   +5 more
openaire   +1 more source

Sonic Boom Minimization Through a Simplified Approach for the Preliminary Design of Civil Supersonic Aircraft

16th AIAA/CEAS Aeroacoustics Conference, 2010
In this paper a simple approach aimed to the definition of a supersonic configuration optimized in terms of sonic boom signature will be presented. This approach is based on the application of Carlson’s method that is a simplified method for the calculation of sonic -boom characteristics for a wide variety of supersonic airplane configurations and ...
SCARSELLI, Gennaro, F. Marulo
openaire   +3 more sources