Results 91 to 100 of about 31,952 (223)
A first-order time-domain Green's function approach to supersonic unsteady flow [PDF]
A time-domain Green's Function Method for unsteady supersonic potential flow around complex aircraft configurations is presented. The focus is on the supersonic range wherein the linear potential flow assumption is valid.
Freedman, M. I., Tseng, K.
core +1 more source
Trade Studies Relating to a Long Range Mach 2.6 Supercruiser [PDF]
A systems study was conducted on an aircraft concept, representative of a supersonic-cruise military aircraft (supercruiser). The study results indicate that supersonic ranges in excess of 4000 n.mi.
Foss, W. E., Jr., Sorrells, R. B., III
core +1 more source
Wind tunnel evaluation of YF-12 inlet response to internal airflow disturbances with and without control [PDF]
, 1978 The response of terminal-shock position and static pressures in the subsonic duct of a YF-12 aircraft flight-hardware inlet to perturbations in simulated engine corrected airflow were obtained with and without inlet control.
Cole, G. L. +2 more
core +1 more source
Supersonic through-flow fan engine and aircraft mission performance [PDF]
A study was made to evaluate potential improvement to a commercial supersonic transport by powering it with supersonic through-flow fan turbofan engines. A Mach 3.2 mission was considered.
Franciscus, Leo C., Maldonado, Jaime J.
core +1 more source
Variable sweep aircraft Patent [PDF]
, 1970 Development and characteristics of variable sweep wing control system for supersonic ...
Hammond, A. D., Polhamus, E. C.
core +1 more source
Optimal design for low sonic boom based on CoKriging surrogate model
Hangkong gongcheng jinzhanAccurately predicting and effectively reducing sonic boom levels is one of the key issues in the development of the new generation of green supersonic civil aircraft.
ZHANG Hanqi, XU Yue, ZHONG Min, LI Yan
doaj +1 more source
The atmospheric effects of stratospheric aircraft: A current consensus [PDF]
In the early 1970's, a fleet of supersonic aircraft flying in the lower stratosphere was proposed. A large fleet was never built for economic, political, and environmental reasons.
Carroll, M. A. +6 more
core +1 more source
Application of computational fluid dynamics and laminar flow technology for improved performance and sonic boom reduction [PDF]
, 1992 A discussion is given of the many factors that affect sonic booms with particular emphasis on the application and development of improved computational fluid dynamics (CFD) codes.
Bobbitt, Percy J.
core +1 more source
Гуманитарные и юридические исследования, 2021 This article discusses the main activities of the outstanding Soviet aircraft designer - A. S. Moskalev, who became a worthy successor of the national school of aeronautical engineering, which passed to him from I. Sikorsky through N. N. Polikarpov.
V. Gagin
doaj
Evaluation of liquid methane storage and transfer problems in supersonic aircraft [PDF]
Evaluation of liquid methane storage and transfer problems for future supersonic aircraft cryogenic fuel ...
Brady, H. F. +3 more
core +1 more source