Opening book details…
Can I read Extended measurements of aerodynamic stability and limb dislodgement forces with the ACES II ejection seat on EtoBox?
Extended measurements of aerodynamic stability and limb dislodgement forces with the ACES II ejection seat by Hawker, Fred W., is a nonfiction available to read on EtoBox.
What is Extended measurements of aerodynamic stability and limb dislodgement forces with the ACES II ejection seat about?
The ACES-2 seat was mounted in a wind tunnel in various attitudes of pitch and yaw. The hand and foot rests were equipped with means to measure limb dislodgement forces. Overall forces and moments were measured at the seat mount. Human subjects were used as seat occupants for gross force and moment data on the seat/occupant combination, as well as limb dislodgement force measurements. Anthropomorphic dummies were used for an extended range of yaw angles around to 180 degrees. Only gross force and moment data for the seat/occupant combination were taken with the dummy subjects. The limb dislodgement results are complementary to earlier tests at low pitch angles and show general reductions in magnitude as the pitch angle is increased
Who reads Extended measurements of aerodynamic stability and limb dislodgement forces with the ACES II ejection seat?
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Hawker, Fred W.,
- Publisher
- Aerospace Medical Research Laboratory, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1975.
- Published
- 1975
- Language
- EN
- Category
- nonfiction
More by Hawker, Fred W.,
Browse all works by Hawker, Fred W.,
Similar books
- Aerodynamic Characteristics of an Ejection Seat Escape System with a Stabilization Parachute at Mach Numbers from 0.3 Through 1.2 — Reichenau, David E. A., (1972)
- Wake Properties Behind an Ejection Seat Escape System and Aerodynamic Characteristics with Stabilization Parachutes at Mach Numbers from 0.6 to 1.5 — Reichenau, David E. A., (1971)
- The Influence of Vertical-tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model with One Engine Inoperative — Pitkin, Marvin. (1945)
- Experimental Verification of the Rudder-free Stability Theory for an Airplane Model Equipped with Rudders Having Negative Floating Tendency and Negligible Friction — McKinney, Marion O. (1944)
- Influence of Wind Tunnel Noise on the Location of Boundary-layer Transition on a Slender Cone at Mach Numbers from 0.2 to 5.5. Volume II, Tabulated and Plotted Data / N. Sam Dougherty, Jr. — Dougherty, N. Sam, Jr., (1980)
- Theoretical Prediction of Pressures in Hypersonic Flow with Special Reference to Configurations Having Attached Leading-edge Shock. Part III, Experimental Measurements of Forces at Mach 8 and Pressures at Mach 21 / Harold R. Mead, Frank Koch, Stavros A. Hartofilis. — Harold R Mead; Frank Koch; Stavros A Hartofilis; Grumman Aircraft Engineering Corporation.; United States. Air Force. Systems Command. Aeronautical Systems Division (1962)