[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

LEMAITRE, 1962 - Google Patents

Theoretical investigation of the use of components in the plastic range to obtain lighter aircraft structures

LEMAITRE, 1962

Document ID
6082078698605388780
Author
LEMAITRE J
Publication year

External Links

Continue reading at scholar.google.com (other versions)

Similar Documents

Publication Publication Date Title
Mitchell The study of chromaticism
LEMAITRE Theoretical investigation of the use of components in the plastic range to obtain lighter aircraft structures
WALLOUCH Examination of the structural aspects of supersonic transport aircraft
ASCHOFF Anisotropy of the skin in respect to thermo- conductivity
SPILLMAN Design and performance requirements of man-powered aircraft
MOORE Jet-lift v/stol military aircraft development in the united kingdom
FLAX Aircraft aerodynamics research
GOLDBERG Solution of equations of motion for the general theory of relativity using the einstein-infeld- hoffmann approximation as compared to other approximation methods
SAELMAN Effect of wing geometry on wing weight and fuel volume
RAJPERT Problems of airfield construction with respect to the accommodation of modern airplanes and helicopters
STEINER Discussion of the design and development of the boeing 727 aircraft
KRASOVSKIY Studies of the upper atmosphere- aurora and airglow
MANDEL Investigation of the basic phenomena defining plasticity
Hiatt et al. Radar Cross-Section of the B-70 Aircraft
DEUTSCH Study of the saint-venant torsion problem corresponding to certain sections resembling airfoil sections
Dong et al. Studies relating to structural analysis of solid propellants
RAJPERT Airport design to meet the requirements of modern air transportation
Roberts Development of the 9 ks 11000 black brant iii rocket engine
Cope The 1654 Edition of Emmanuele Tesauro's II cannochiale aristotelico
MARTIN Unofficial records of research rocket airplanes with physical characteristics
KRAUS Formulation of the stability problem for double- symmetric and quasi-flat profiles using an integral equation
STUSSEL Comparison of vertical takeoff aircraft with the conventional type
KRECISZ Structural model of gyroscope with three degrees of freedom
TAYLOR Description of blood typing to provide assistance to the aircraft accident investigator
REICHEL Effect of airframe elasticity upon static longitudinal stability