Cover Image

Bio-assay techniques for human centrifuges and physiological effects of acceleration

Corporate Author:	North Atlantic Treaty Organization Advisory Group of Aeronautical Research and Development
Other Authors:	Bergeret, P.
Format:	Book
Language:	English
Published:	New York Pergamon 1961
Subjects:	Αεροπλάνα, Στρατιωτικά

Similar Items

Slip flow testing techniques
Published: (1959)

Ground effect machines
Published: (1962)

Corner interference effects Report 299
Published: (1959)

Review of the effect of distributed surface [report 254] : roughness on boundary - layer transition
Published: (1960)

Effect of roughness on transition in supersonic flow Report 255
Published: (1960)

Cyclic temperature effects on materials and structures Report 410
Published: (1962)

Flight test techniques and instrumentation for VTOL aircraft Report 319
Published: (1961)

Effects of servo-mechanism characteristics on aircraft stability and control Report 361
Published: (1961)

Consideration of human factors in helicopter design Report 238
Published: (1959)

Some human engineering aspects of several unconventional aircraft
Published: (1959)

Non - aeronautical applications of low-speed wind tunnel techniques Report 313
Published: (1960)

Tunnel-wall effects associated with VTOL-STOL model testing Report 303
Published: (1959)

The effect on profile drag of randomly distributed, low - intensity roughness Report 257
Published: (1960)

Some effects of internal heat sources on the design of flight structures Report 208
Published: (1958)

Physiological instrumentation of pilots for test and operational flights in navy high performance jet aircraft Phase I - Preliminary investigations : Report 240
Published: (1959)

Large angle of attack model - sting interference effects at transonic speeds Report 301
Published: (1959)

Effects of unit Reynolds number, nose bluntness, and roughness on boundary layer transition Report 256
Published: (1960)

Medical and human engineering aspects of flight in man VTOL and STOL airgraft
Published: (1959)

Some effects of wind tunnel interference observed in tests on two-dimensional aerofoils at high subsonic and transonic speeds Report 296
Published: (1959)

An investigation of interference effects on similar models of different size in various transonic tunnels in the United Kingdom Report 297
Published: (1959)

Effects of heat transfer on laminar boundary layer development under pressure gradients in compressible flow Report 279
Published: (1960)

The effectiveness of the transonic wind tunnel as a device for minimizing tunnel - boundary interference for model tests at transonic speeds Report 294
Published: (1959)

An experimental technique to measure heat transfer fluxes at high speeds:Turbulent heat transfer data on a blunt body at M=3.98 Report 284
Published: (1960)

Flight testing of the Fiat G91 Report 315
Published: (1961)

Aliasing errors in sampled data systems Report 316
Published: (1961)

Flight test instrumentation for V/STOL aircraft Report 317
Published: (1961)

Some notes on United Kingdom experience in the testing of VTOL aircraft Report 318
Published: (1961)

The place of servo-mechanisms in the design of aircraft with good flight characteristics Report 360
Published: (1961)

Escape and survival:Clinical and biological problems in aero space medicine
Published: (1961)

The use of piloted flight simualtors in general research
Published: (1961)

The influence of aerodynamics in wind power development Report 401
Published: (1961)

Law noise electronics Avionics Panel conference
Published: (1961)

A review of measurements on AGARD calibration models
Published: (1961)

Gas sampling and chemical analysis in combustion processes
Published: (1961)

Transonic wind tunnel testing
Published: (1961)

Niobium, molybdenum, tantalum and tungsten A summary of their properties with recommendations for research and development
Published: (1961)

Fundamental data obtained from shock-tube experiments
Published: (1961)

The flight testing of aircraft weapon systems Report 287
Published: (1960)

The thermal laminar boundary layer on a rotating sphere Report 283
Published: (1960)

Design and operation of the X-15 hypersonic research airplane Report 288
Published: (1960)

Cannot write session to /tmp/vufind_sessions/sess_84qeqegb69cordi81o02frdfq0