CĂRȚI ÎN ENGLEZĂ ÎN LEGĂTURĂ CU «SWEEPBACK»
Descoperă întrebuințarea
sweepback în următoarea selecție bibliografică. Cărți în legătură cu
sweepback și extrase din aceasta pentru a furniza contextul de întrebuințare al acestuia în literatura Engleză.
1
Pilot's Handbook of Aeronautical Knowledge, 2009
This is the primary reason for the development of the T-tail configuration on many
turbine-powered aircraft, which places the horizontal stabilizer as far as practical
from the turbulence of the wings. Sweepback Most of the difficulties of transonic ...
Transportation Department, Federal Aviation Administration, Flight Standards Service
2
Eshbach's Handbook of Engineering Fundamentals
6.66 Effect of compressibility and sweepback on drag of NACA 00012 airfoil with
aspect ratio 6. component perpendicular to the leading edge (l^.cosALE) is less
than free-stream velocity; it is this component that determines the magnitude of ...
Ovid Wallace Eshbach, Byron D. Tapley, Thurman R. Poston, 1990
3
Synthesis of Subsonic Airplane Design: An Introduction to ...
Angle of sweepback. The previous section has made it clear that the wing
sweepback should not be more than the minimum required. For cruising speeds
of up to about M - .65 to .70 compressibility effects can be catered for with a
straight ...
4
Pilot's Handbook of Aeronautical Knowledge
A detailed index and full glossary make this book easy to navigate and useful in quick reference situations.
Federal Aviation Administration, 2009
How a straightedge and a scale are used to measure the sweepback of a model
airplane wing. The scale should be ... Some wings embody all these points, while
others may, or may not, have camber, dihedral, or sweepback. Any plans from ...
by E. COLSTON SHEPHERD SINCE the Swallow, the variable sweepback
aeroplane designed by Dr. Barnes Wallis, passed into the hands of the Mutual
Aid Authority, with United States and British Government finance behind it, the
project ...
7
Biomechanics and Medicine in Swimming IX: Proceedings of the ...
maximum thrusts are obtained at a=90° different from The maximal values of
characteristics 77, CT are plotted as a function of sweepback angle f in Fig. 7(a)
and (b). The results are: (i) The maximum thrust can be obtained when #=90° or ...
Jean-Claude Chatard, 2003
8
Aerodynamics: Selected Topics in the Light of Their ...
He had heard of Robert Jones's ideas about sweepback, but the Volkenrode data
were the first experimental results he had seen. It is related that Schairer wired
back to his home office: "Stop the bomber design" and that this led to the birth of ...
Theodore Von Kármán, 2004
9
Principles of Helicopter Aerodynamics with CD Extra
A distinctive feature of the BERP blade is the use of high sweepback over the tip
region, which as mentioned previously, is an effective means of reducing
compressibility effects and delaying their effects on the rotor to a higher advance
ratio.
10
The Encyclopaedia of Sports Medicine: An IOC Medical ...
The form of the propelling segment and the sweepback angle also influence the
magnitude of CDX and FD at different angles of attack (Table 10.2). Normal
component of hydrodynamic reaction— hydrodynamic lift (L) Streamlining of the
hand ...
