Maciejczyk et al., 1974 - Google Patents
Degree of reaction and decision taking of the pilot in stress situationsMaciejczyk et al., 1974
- Document ID
- 2485018278793936559
- Author
- Maciejczyk J
- TERELAK J
- Publication year
- Publication venue
- (Polskie Towarzystwo Astronautyczne, Konferencja Naukowa Poswiecona Wspolczesnym Zagadnieniom Astronautyki, Augustow, Poland, Sept. 27-29, 1973.) Postepy Astronautyki,
External Links
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Scruton | The use of wind tunnels in industrial aerodynamic research | |
Maciejczyk et al. | Degree of reaction and decision taking of the pilot in stress situations | |
Davidson et al. | The effect of barrier shape in the rate theory of metal plasticity(based on crystal dislocations) | |
Clingan | Rapid method for determining wind shear design loads based on a set of measured profiles | |
Walles et al. | On the extrapolation and scatter of creep data | |
AKISTER | Ariane interstage 2/3: Stress analysis- first loop(FEA-1)(finite element displacement analysis) | |
KARLASHOV et al. | Differentiation of corrosion damage by the severity of its effects upon the resistance to fatigue and corrosion-fatigue disintegration of aircraft skin elements | |
Newberry | The treatment of interaction of handling qualities, stability, and control on structural loads by current specifications[Summary Report] | |
Herrouin et al. | General survey of the studies and testing techniques that led to the definition of N 500 performance | |
HUNTLEY | Wind tunnel tests at transonic and supersonic speeds to investigate the longitudinal stability of a model of the AVRO 720 aircraft(Wind tunnel longitudinal stability tests of AVRO 720 scale model with determination of up-elevon and leading edge notch effects) | |
FATKHULLIN et al. | Transient processes in stabilization system of flight vehicle with reaction flywheels | |
WHORIC | Effect of various external stores on the aerodynamic characteristics of the F-4 C aircraft[Final Report, 10 Sep.- 13 Oct. 1973] | |
KUBIS et al. | Time and motion, experiment M 151(human performance and space flight stress) | |
Carr et al. | Aircrew restraint system: Design criteria evaluation[Final Report, Apr. 1973- Feb. 1975] | |
ROOD | Estimated hydrodynamic strut side forces on a 200-ton 80 knot hydrofoil craft[Interim Report] | |
Starzhinskii | Several methods for nonlinear oscillations- Theory and application | |
NIBLETT | The flutter of a two-dimensional wing with simple aerodynamics(forces) | |
JOSEPH | Comparison of the flying qualities of the A-7 D aircraft with the requirements of MIL-F-8785 B ASG[Technical Report, Mar.- Dec. 1972] | |
CLELLAN | Fatigue lessons learnt from the argosy(Fatigue performance of peripheral crack stoppers and deep frames with intercostal stringers, used in the aw 650 argosy) | |
MEANS | Economic and social aspects of weather modification | |
KOBYLKA | Design and production of high-temperature resistance strain gages with experience gained by testing on gas-turbine blades | |
PANASIUK et al. | The limiting equilibrium state of a strip with a crack | |
DODSON et al. | Advanced cost estimating and synthesis techniques for avionics[Final Report] | |
BUINA et al. | Determination of the critical crack angle(for elastic strip under tension) | |
JU et al. | Couple-stress to an infinite plate bounded by an elliptical hole with static equilibrating tractions(Mathieu functions for solving stress problems of infinite plate bounded by elliptical hole with equilibrating tractions) |