WorldCat Identities

Cooper, George E.

Overview
Works: 42 works in 69 publications in 1 language and 540 library holdings
Genres: Conference papers and proceedings 
Roles: Author
Classifications: RT86.73, 331.126
Publication Timeline
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Most widely held works by George E Cooper
MOVANAID, an interactive aid for analysis of movement capabilities by George E Cooper( Book )

4 editions published in 1978 in English and held by 212 WorldCat member libraries worldwide

A computer-drive interactive aid for movement analysis, called MOVANAID, has been developed and is described in this report. The aid, which has been designed to be of assistance in the performance of certain Army intelligence processing tasks in a tactical environment, can compute fastest travel times and paths through road networks for military units of various types, as well as fastest times in which simultaneous maneuvers of certain types can be completed. Military situations in which the aid might be useful are discussed, and the manner in which users interact with the aid is described. Details about the analytic basis upon which the aid has been constructed, together with a discussion of the method in which the aid has been computer implemented, are also given. Ideas for ways in which the capabilities of the aid can be extended are discussed. (Author)
The impact of health system changes on the nation's requirements for registered nurses in 1985 by Timothy C Doyle( Book )

2 editions published in 1978 in English and held by 182 WorldCat member libraries worldwide

A piloted simulation study of operational aspects of the stall pitch-up by Maurice D White( )

3 editions published in 1967 in English and held by 29 WorldCat member libraries worldwide

Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method by Jim Rogers Thompson( )

2 editions published in 1950 in English and held by 24 WorldCat member libraries worldwide

Of the systems investigated, a nose-boom installation was found to be most suitable for research use at transonic and low supersonic speeds because it provided the greatest sensitivity of the indicated Mach number to a unit change in true Mach number at very high subsonic speeds, and because it was least sensitive to changes in airplane normal-force coefficient. The static-pressure error of the nose-boom system was small and constant above a Mach number of 1.03 after passage of the fuselage bow shock wave over the airspeed head
The use of piloted flight simulators in take-off and landing research by George E Cooper( Book )

2 editions published in 1963 in English and held by 11 WorldCat member libraries worldwide

The use of piloted simulators in research and as a technique for aircraft development is discussed from the pilot's viewpoint. An attempt is made to examine both the advantages and the limitations encountered in their use. Several factors which affect significantly the validity of the research results drawn from piloted simulators arediscussed in some detail. These include: control system characteristics, visual cues related to cockpit instruments and those related to the outside world, motion cues or distractions, selection of criteria and tasks, environmental and operational aspects, and fidelity of the analog simulation. Examples of the use of piloted simulators in landing research are presented and discussed with the purpose of illustrating and defining both their value and limitation with respect to those six items. Future objectives and applications in the area of take-off and landing research by means of piloted simulation are outlined. (Author)
Resource management on the flight deck : proceedings of a NASA/Industry workshop held at San Francisco, California, June 26-28, 1979 by NASA/Industry Workshop( Book )

6 editions published between 1979 and 1980 in English and held by 8 WorldCat member libraries worldwide

The impact of health system changes on the nation's requirements for registered nurses in 1985 by Timothy C Doyle( Book )

3 editions published in 1978 in English and Undetermined and held by 6 WorldCat member libraries worldwide

Schlieren investigation of the wing shock-wave boundary-layer interaction in flight by George E Cooper( Book )

2 editions published in 1951 in English and held by 6 WorldCat member libraries worldwide

This report presents the data obtained in flight using a schlieren apparatus which photographed the shock-wave interaction with a thick turbulent boundary layer on a wing. Local Mach number and boundary-layer characteristics obtained from pressure measurements in the vicinity of the shock wave are also presented
Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 ̊swept-wing airplane by Woodrow L Cook( Book )

4 editions published in 1958 in English and Undetermined and held by 6 WorldCat member libraries worldwide

Flight measurements of the effect of a controllable thrust reverser on the flight characteristics of a single-engine jet airplane by Seth B Anderson( Book )

1 edition published in 1959 in English and held by 5 WorldCat member libraries worldwide

A comparison of the measured and predicted lateral oscillatory characteristics of a 35 degree swept-wing fighter airplane by Walter E McNeill( Book )

2 editions published between 1951 and 1955 in English and held by 4 WorldCat member libraries worldwide

The airplane was found to be laterally stable, statically and dynamically, throughout the range of speeds tested. At both altitudes, the variation with Mach number of the period of the lateral oscillation was satisfactorily predicted from available and estimated aerodynamic and mass parameters. The time required to damp to half amplitude, as measured from flight at both altitudes, varied with Mach number in essentially the same manner as predicted from computations. The measured damping was somewhat better than that obtained from computations for the altitude of 35,000 feet, particularly at a Mach number of 0.92. An increase in time to damp to half amplitude was noted between Mach numbers of 0.95 and 1.04
An evaluation of the factors which influence the selection of landing approach speeds by Fred J Drinkwater( Book )

1 edition published in 1958 in English and held by 4 WorldCat member libraries worldwide

Flight observations of aileron flutter at high mach numbers as affected by several modifications by John R Spreiter( Book )

3 editions published in 1947 in English and held by 3 WorldCat member libraries worldwide

Preliminary flight investigation of the maneuvering accelerations and buffet boundary of a 35° swept-wing airplane at high altitude and transonic speeds by George A Rathert( Book )

1 edition published in 1951 in English and held by 3 WorldCat member libraries worldwide

A survey of the status of and philosophies relating to cockpit warning systems by George E Cooper( Book )

1 edition published in 1977 in English and held by 2 WorldCat member libraries worldwide

Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method by Jim Rogers Thompson( Book )

2 editions published in 1955 in English and held by 2 WorldCat member libraries worldwide

The calibrations of four airspeed systems installed in a North American F-86A airplane have been determined in flight at Mach numbers up to 1.04 by the NACA radar-phototheodolite method. The variation of the static-pressure error per unit indicated impact pressure is presented for three systems typical of those currently in use in flight research, a nose boom and two different wing-tip booms, and for the standard service system installed in the airplane. A limited amount of information on the effect of airplane normal-force coefficient on the static-pressure error is included. The results are compared with available theory and with results from wind-tunnel tests of the airspeed heads alone. Of the systems investigated, a nose-boom installation was found to be most suitable for research use at transonic and low supersonic speeds because it provided the greatest sensitivity of the indicated Mach number to a unit change in true Mach number at very high subsonic speeds, and because it was least sensitive to changes in airplane normal-force coefficient. The static-pressure error of the nose-boom system was small and constant above a Mach number of 1.03 after passage of the fuselage bow shock wave over the airspeed head
MOVANAID An Interactive Aid for Analysis of Movement Capabilities by George E Cooper( Book )

1 edition published in 1978 in English and held by 2 WorldCat member libraries worldwide

A computer-drive interactive aid for movement analysis, called MOVANAID, has been developed to be of assistance in the performance of certain Army intelligence processing tasks in a tactical environment. It can compute fastest travel times and paths through road networks for military units of various types, as well as fastest times in which simultaneous maneuvers of certain types can be completed. Military situations in which the aid might be useful are discussed, and the manner in which users interact with the aid is described. Details about the analytic basis upon which the aid has been constructed and a discussion of the method used for computer implementation are also given. Possible extensions of the capabilities of the aid are also discussed. (Author/JVP)
The use of pilot rating in the evaluation of aircraft handling qualities by George E Cooper( Book )

1 edition published in 1969 in English and held by 2 WorldCat member libraries worldwide

Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion by Melvin Sadoff( Book )

1 edition published in 1957 in English and held by 2 WorldCat member libraries worldwide

The method of NACA RM A55D06 was used in m analytical study of the comparative pitch-up behavior of six ~et-powered swept-wing airplanes. The effects of several important variables, including recovery control rate, entry rate, and altitude are assessed
The Use of pilot rating in the evaluation of aircraft handling qualities by North Atlantic Treaty Organization( Book )

2 editions published between 1968 and 1969 in English and held by 2 WorldCat member libraries worldwide

 
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Audience level: 0.59 (from 0.52 for MOVANAID, ... to 0.99 for George E. ...)

Languages
English (44)