Emerald
SCOPUS (1929-2025)
0002-2667
Cơ quản chủ quản: Emerald Group Publishing Ltd.
Lĩnh vực:
Aerospace Engineering
Phân tích ảnh hưởng
Các bài báo tiêu biểu
Optimal trajectory analysis of hypersonic boost-glide waverider with heat load constraint
Tập 87 Số 1 - Trang 67-78 - 2015
Trajectory optimization for hypersonic boost‐glide missile considering aeroheating
Tập 81 Số 1 - Trang 3-13 - 2009
PurposeThe purpose of this paper is to optimize the downrange for hypersonic
boost‐glide (HBG) missile under near‐real condition, and to validate the
suitability of proposed wall cooling materials.Design/methodology/approachThe
trajectory optimization problem is characterized by a boost phase followed by a
glide phase. A multi‐phase trajectory optimization tool is adopted to optimize
the downrange...
Factors Affecting Stress Formation in Glass During the Toughening Process
Tập 36 Số 12 - Trang 392-394 - 1964
The mechanism of stress formation in glass under‐going conditions of rapid
cooling, and the factors affecting the properties of the toughened glass
produced are discussed. The application of techniques for measuring the
temperature of glass, to the control and study of the toughening process are
described.
Simple autopilot design procedure based on a factorization approach
Tập 78 Số 5 - Trang 407-414 - 2006
PurposeThe purpose of this paper is to apply a factorization‐based control
system design procedure to design of auto‐pilot
systems.Design/methodology/approachThe design approach is based on a previously
developed factorization‐based control system design procedure. The design
approach requires a stable coprime factorization of the plant, a set of stable
coprime factors that are solutions to the Be...
Research Reports and Memoranda
Tập 4 Số 1 - Trang 23-25 - 1932
Under this heading are published regularly abstracts of all Reports and
Memoranda of the Aeronautical Research Committee, Reports and Technical Notes of
the U.S. National Advisory Committee for Aeronautics, and publications of other
similar research bodies as issued
The All‐Metal Blackburn “Bluebird” Mark IV
- 1929
THE experience gained with the previous models of the “Bluebird” type has
enabled the Bluebird IV to be produced embodying all the requirements essential
in a light aeroplane for private and club flying. This experience indicated that
the policy of side‐by‐side seating in preference to the more usual tandem
arrangement was fully justified, and, although previously it had been considered
that such ...
Discontinuity Stresses in Stiffened Cylindrical Shells
Tập 31 Số 5 - Trang 131-132 - 1959
THIN cylindrical shells stiffened at intervals along their length by internal
frames or bulkheads are often used in fuselage design. When such shells are
pressurized or heated, expansion of the shell results and, unless the subsequent
deformations of shell and stiffeners are equal, discontinuity stresses are
induced in the region of the shell‐stiffener joint making all the deformations
compatible.