WorldCat Identities

Crane, H. L.

Overview
Works: 34 works in 69 publications in 1 language and 185 library holdings
Roles: Author
Classifications: S21, 630
Publication Timeline
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Most widely held works by H. L Crane
Nutrient element balance : response of tung trees grown in sand culture to potassium, magnesium, calcium, and their interactions by C. B Shear( Book )

6 editions published in 1953 in English and held by 39 WorldCat member libraries worldwide

Low-speed flight investigation of a jet transport with a powered-lift boundary-layer control system by R. O Schade( Book )

5 editions published in 1965 in English and Undetermined and held by 13 WorldCat member libraries worldwide

Physiological Investigations on the Resistance of Peach Buds to Freezing Temperatures by H. L Crane( Book )

5 editions published in 1930 in English and held by 11 WorldCat member libraries worldwide

Orchard management and cost of pecan production by R. S Washburn( Book )

1 edition published in 1942 in English and held by 9 WorldCat member libraries worldwide

Experiments in Fertilizing Peach Trees by H. L Crane( Book )

3 editions published in 1924 in English and held by 9 WorldCat member libraries worldwide

The Effect of Height of Head on Young Apple Tree Growth and Yield by H. L Crane( Book )

4 editions published in 1928 in English and held by 6 WorldCat member libraries worldwide

The Fertilization of Apple Orchards by W. H Alderman( Book )

3 editions published in 1920 in English and held by 5 WorldCat member libraries worldwide

A Study of Factors Governing the Efficiency of Distribution and Rate of Discharge of Spray Nozzles by H. L Crane( Book )

2 editions published in 1919 in English and held by 5 WorldCat member libraries worldwide

Effects of Pruning on Growth and Yield of Cherry Trees by H. L Crane( Book )

3 editions published in 1931 in English and held by 5 WorldCat member libraries worldwide

Effect of lateral shift of center of gravity on rudder deflection required for trim by W. H Phillips( Book )

5 editions published in 1944 in English and held by 5 WorldCat member libraries worldwide

Tests of a single-engine scout-bomber airplane showed that the rudder deflection required for trim at low speed in the critical wave-off condition may be reduced approximately 10 degrees by a lateral shift of the center of gravity equal to 1.8 percent of the wing span. The reduction in rudder deflection required to offset yawing moments from the ailerons and from the component of the weight in the direction of the longitudinal axis and the rudder deflection required to hold the sideslip angle necessary to maintain straight flight. The effect of the lateral loading must be taken into account in tests to determine the adequacy of the rudder for trim. The lateral center-of-gravity location is also important in the service operation of airplanes because, by suitable distribution of the useful load in the wings, the ability of the rudder to trim the airplane in critical power-on conditions may be markedly improved
Orchard and Garden Spraying by H. L Crane( Book )

2 editions published in 1914 in English and held by 4 WorldCat member libraries worldwide

Formation of the Detroit Freeway Operations Unit by H. L Crane( Book )

2 editions published in 1969 in English and held by 4 WorldCat member libraries worldwide

Matrix Bandwidth and Profile Reduction( Book )

2 editions published in 1975 in English and held by 3 WorldCat member libraries worldwide

This program, REDUCE, reduces the bandwidth and profile of sparse symmetric matrices, using row and corresponding column permutations. It is a realization of the algorithm described by the authors elsewhere. It was extensively tested and compared with several other programs and was found to be considerably faster than the others, superior for bandwidth reduction and as satisfactory as any other for profile reduction
Measurement of flying qualities of a Dehavilland Mosquito F-8 airplane (AAF No. 43-334960). 1 - Lateral and directional stability and control characteristics by H. L Crane( Book )

1 edition published in 1945 in English and held by 3 WorldCat member libraries worldwide

The data presented have no bearing on performance characteristics of airplane, which were considered exceptionally good in previous tests. Some of the undesirable features of lateral and directional stability and control characteristics of the F-8 are listed. Directional stability, with rudder fixed, did not sufficiently restrict aileron yaw; rudder control was inadequate during take-off and landing, and was insufficient to fly airplane with one engine; in clean condition, power of ailerons was slightly below minimum value specified; it was difficult to trim airplane in rough air
Longitudinal stability and control characteristics by H. L Crane( Book )

2 editions published between 1944 and 1945 in English and held by 2 WorldCat member libraries worldwide

Measurement of flying qualities of a Douglas A-26B airplane (AAF by H. L Crane( Book )

2 editions published between 1944 and 1945 in English and held by 2 WorldCat member libraries worldwide

Flight tests of various tail modifications on the Brewster XSBA-1 airplane. 2 - Measurements of flying qualities with tail configuration Number Two by W. H Phillips( Book )

1 edition published in 1943 in English and held by 2 WorldCat member libraries worldwide

Several tail modifications of the Brewster XSBA-1 scout-bomber were investigated and results compared. Modifications consisted of variation of the chord of the elevator and rudder while the total area of the surfaces is kept constant and variations of the total area of the vertical tail surface. Configuration number 2 reduced trim changes by 50 percent and reduced average elevator control force gradient from 30 to 27 pounds/g. Stick travel required to stall in maneuver was 4.6 inches
Flight tests of various tail modifications on the Brewster XSBA-1 airplane. 3 - Measurements of flying qualities with tail configuration 3 by H. L Crane( Book )

1 edition published in 1944 in English and held by 2 WorldCat member libraries worldwide

Three tail configurations of the Brewster XSBA-1 scouting bomber were flight tested. One had approximately equal movable surfaces and horn balances; another had identical surfaces but was not horn-balanced. The elevator area of the third configuration was reduced to about 25 percent of the total horizontal area, and rudder area was reduced 35 percent of the total vertical-tail area. Results of the third design of narrow-chord movable surfaces are presented and compared with previously obtained results on the other two configurations of wide-chord movable surfaces
Measurement of Flying Qualities of a DeHavilland Mosquito F-8 Airplane (AAF No. 43-334960). 1 - Lateral and Directional Stability and Control Characteristics( Book )

2 editions published in 1945 in English and held by 1 WorldCat member library worldwide

The data presented have no bearing on performance characteristics of airplane, which were considered exceptionally good in previous tests. Some of the undesirable features of lateral and directional stability and control characteristics of the F-8 are listed. Directional stability, with rudder fixed, did not sufficiently restrict aileron yaw; rudder control was inadequate during take-off and landing, and was insufficient to fly airplane with one engine; in clean condition, power of ailerons was slightly below minimum value specified; it was difficult to trim airplane in rough air
Simultaneous independent parallel approaches in Canada using modernized sensors and displays by Canada( Book )

2 editions published in 1995 in English and held by 1 WorldCat member library worldwide

Transport Canada has recently completed the Radar Modernisation Programme (RAMP), which was a project to install 22 Terminal Surveillance Radars and 17 Independent Secondary Surveillance Radars, as well as Radar Data Processing Systems and Display Equipment for seven Area Control Centres and two Terminal Control Units. The RAMP Radar and Display System provides a significant increase in surveillance accuracy, display, and processing over earlier radar and display systems. At the request of Transport Canada, the Center for Advanced Aviation System Development (CAASD) at The MITRE Corporation analyzed the RAMP Radar and Display System and Canadian ATC procedures to estimate the potential for refining standards for simultaneous independent parallel ILS approaches. Conclusions are that the system has the potential to allow reduction in minimum runway spacing with some changes to current procedures. Further testing to verify the reduction is recommended, and suggestions for further improvements are included. Analysis and recommendations are also conducted for the Canadian Automated Air Traffic System (CAATS)
 
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Audience level: 0.77 (from 0.67 for Measuremen ... to 0.99 for Measuremen ...)

Languages
English (53)