 |
||||||||||||||||||||||||||||||||||||||||||||||||
|
||||||||||||||||||||||||||||||||||||||||||||||||
| |||||||||||||||||||||||||||||||||||||||||||||||||||
|
 Journal of The American Helicopter Society 1966 January 11, 1 “Publish Or Die -- Technical Director's Editorial”, by Ellis, Charles W., Pgs 1 “Some Fundamentals for Efficient VTOL Aircraft Hover Control”, by Hill, Gardner T., Lockheed-Georgia Co., Pgs 2 “The Influence of Lightning and Static Electricity on Helicopter Design”, by Solak, B. J., The Boeing Co., Pgs 10 “Ureka - A Vibration Balancing Device for Helicopters”, by Hooper, Euan W., The Boeing Co., Pgs 28 1966 April 11, 2 “Thrust Response; A Lift Engine Problem?”, by Richardson, Harry L., Curtiss-Wright Corp., Pgs 8 “Prop-Rotor Stability at High Advance Ratios”, by Hall, Jr., W. Earl, Bell Helicopter Co., Pgs 11 “A Variable Speed Constant Frequency Generating System For Helicopter Applications”, by Lawson, Louis J., Lear Siegler, Inc., Pgs 27 1966 July 11, 3 “Experimental Boundary Layer Study on Hovering Rotors”, by Tanner, W. H., Bell Helicopter Co., Yaggy, P. F., Pgs 22 “Helicopter Trainee Performance Following Synthetic Flight Training”, by Caro, Jr., Paul W., Isley, Robert, Pgs 38 “Concepts and Techniques for Helicopter Airframe Fatigue Tests”, by Lane, Walter A., Sikorsky Aircraft Corp., Pgs 45 1966 October 11, 4 “An Improved Computational Model For Predicting the Unsteady Aerodynamic Loads of Rotor Blades”, by Daughaday, H., Cornell Aeronautical Laboratory, Inc., Piziali, R. A., Pgs 3 “Helicopter Rotor Blade Radar Antenna”, by Upton, Hugh W., Bell Helicopter Co., Pgs 11 “Vibrations of a Rotating Beam”, by Lipeles, Jay L., Martin Co., Pgs 17 1967 January 12, 1 “Analysis of Stowed Rotor Aeroelastic Characteristics”, by Donham, Robert E., Lockheed-California Co., Harvick, Wayne P., Pgs 21 “An Analysis of The Divergent Vertical Helicopter Oscillations Resulting From the Physical Presence of the Pilot in the Collective Control Loop”, by Lytwyn, Roman T., The Boeing Co., Pgs 45 1967 April 12, 2 “U.T.M. Grid Navigation By Doppler-Inertial Airborne Gyrocompassing”, by Buell, Heinz, General Precision, Inc., Reed, William, Pgs 14 “Suggested Requirements For Military Helicopter Gas Turbine Engine Operating Characteristics”, by Anderson, William A., Ryan Aeronautical Co., Pgs 26 “Angle-of-Attack Distribution of a High Speed Helicopter Rotor”, by Madden, Paul A., Massachusetts Institute of Technology, Pgs 41 1967 July 12, 3 “The Effects of Flight Dynamics on Rotor Blade Antenna Performance”, by Gruber, Robert, Lockheed Electronics Co., Woltornist, Victor, Pgs 16 “CH-54A Engine Inlet Air Particle Separator”, by Stephenson, Carl D., US Army, Shohet, Herbert N., Pgs 26 “Helicopter Cargo Restraint”, by Vichness, Jules A., US Army, House, Thomas, Pgs 41 “Estimating the Reliability of Fatigue Loaded Rotorcraft Structures”, by Nord, Carl E., Sikorsky Aircraft, Pgs 48 “A Comparison of Fatigue Life and Reliability From Constant and Variable Amplitude Loading Tests”, by Davis, Caleb S., Lockheed-California Co., Young, Louis, Pgs 65 1967 October 12, 4 “Stall Flutter of Helicopter Rotor Blades: A Special Case of the Dynamic Stall Phenomenon”, by Ham, Norman D., Massachusetts Institute of Technology, Pgs 19 “Structural Dynamic Response of Large Logistic V/STOL Aircraft”, by Rich, Melvin J., Sikorsky Aircraft Corp., Stebbins, Richard F., Pgs 22 “The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller-Rotors”, by Young, Maurice I., The Boeing Co., Lytwyn, Roman, Pgs 38 “Review and Discussion of 'The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller-Rotors'”, by Wernicke, Kenneth G., Bell Helicopter Co., Gaffey, Troy, Pgs 55 “Response Characteristics of the Gyro-Controlled Lockeed Rotor System”, by Sissingh, G. J., Lockheed-California Co., Pgs 61 “Control Loads and Their Effects on Fuselage Vibrations”, by Kidd, D. L., Bell Helicopter Co., Spivey, R.; Lawrence, K., Pgs 78 “Comments on 'Effects of Control Loads on Fuselage Vibration by D. Kidd, R. Spivey, K. Lawrence'”, by Mard, Kenneth C., Sikorsky Aircraft, Pgs 92 1968 January 13, 1 “Remarks on Dynamic Problems of Composite Aircraft”, by Hohenemser, Kurt, Washington University, Pgs 11 “VTOL Advances as Determined From Analysis of Future Needs and Technological Potentials”, by Lindenbaum, Bernard, US Air Force, Mabli, Robert, Pgs 14 “Considerations of the Stopped Rotor V/STOL Concept”, by Deckert, Wallance H., NASA, McCloud III, John L., Pgs 27 “Flight Program on the NH-3A Research Helicopter”, by Fradenburgh, Evan A., Sikorsky Aircraft, Chuga, Gregory, Pgs 44 “The US Army Huey Cobra Configuration and Design Considerations”, by Seibel, Charles M., Bell Helicopter Co., Pgs 63 “Methods for Improving Flying Qualities of Compound Aircraft”, by Blackburn, W. E., Kaman Corp., Pgs 71 1968 April 13, 2 “Blade Stall-Half Fact, Half Fiction”, by Harris, Franklin D., The Boeing Co., Pruyn, Richard, Pgs 27 “Dynamic Stall Considerations in Helicopter Rotors”, by Ham, Norman D., Massachuttes Institute of Technology, Garelick, Melvin, Pgs 49 “The Helicopter Rotor at High Mach Numbers”, by Tanner, W. H., Bell Helicopter Co., van Wyckhouse, J. F.; Cancro, Patrick; McCloud, III, John, Pgs 56 “Suppression of Transmitted Harmonic Rotor Loads by Blade Pitch Control”, by Daughaday, H., Cornell Aeronautical Lab., Inc., Pgs 65 1968 July 13, 3 “VTOL Handling Qualities Criteria and Control Requirements - Analysis and Experiment”, by Lollar, Thomas, The Boeing Co., Kriechbaum, Gerhard, Pgs 20 “Control Characteristics of Vectored Thrust V/STOL Vehichles in the Transition Regime”, by Coles, Alan, Textron Co., Pgs 35 “Test Approaches to External Sling Load Instabilities”, by Gabel, Richard, The Boeing Co., Wilson, Gregory, Pgs 44 “Dynamics of Rotors Operating at High Advance Ratios”, by Sissingh, G. J., Lockheed-California Co., Pgs 56 “Experimental Flight Tests of the XH-51A Compound Helicopter”, by Spreuer, W. E., Lockheed-California Co., Pgs 64 “Experience of and Methods to Be Used in Clearing a Jet-Lift Aircraft for Service Use”, by Fisher, Ian, Boscombe Down, Pgs 70 1968 October 13, 4 “Elastomeric Bearing Application to Helicopter Tail Rotor Designs”, by Fagan, C. H., Bell Helicopter Co., Pgs 13 “Power Spectral Density Analysis of V/STOL Aircraft Structures”, by Rich, Melvin J., Sikorsky Aircraft Corp., Israel, Martin; Kenigsberg, Irwin; Cook, Peter, Pgs 24 “Designing for Crashworthiness and Survivability”, by Smith, H. G., Hughes Tools Co., McDermott, J. M., Pgs 38 “An Analytical Appoach to the Determination of Particle Trajectories in a S-Bend Duct with Experimental Verification”, by Leitner, Murray, Lockheed-California Co., Pgs 48 “Allison T63 Regenerative Engine Program”, by Privoznik, Edward, General Motors, Pgs 56 1969 January 14, 1 “Using The Remote Terminal Computer to Enhance Design Capability for Rotary Wing Aircraft”, by Lewis, II, Richard, Lockheed-California Co., Pgs 12 “Development and Test of the BO 105 Rigid Rotor Helicopter”, by Weiland, Emil F., Bolkow GmbH, Pgs 22 “A Self-Excited Rotor Blade Oscillation at High Subsonic Mach Numbers”, by Paul, William F., Sikorsky Aircraft Corp., Pgs 38 “Flying Qualities Considerations in the Design and Development of the Huey Cobra”, by Livingston, C. L., Bell Helicopter Co., Murphy, Mr. R., Pgs 49 “The Application of Fracture Mechanics to the Fail Safety of Rotor Blades”, by Stratton, Warren K., The Boeing Co., White, Richard, Pgs 67 1969 April 14, 2 “Tilt Proprotor Composite Aircraft, Design State of the Art”, by Wernicke, K. G., Bell Helicopter Co., Pgs 10 “Dynamic Stall of Airfoil Sections for High-Speed Rotors”, by Liiva, Jean, The Boeing Co., Davenport, Franklyn J., Pgs 26 “Application of Passive Helicopter Rotor Isolation for Alleviation of Rotor Induced Vibration”, by Schuett, Erich P., Kaman Corp., Pgs 34 “The Effect of Positive Pitch-Flap Coupling (Negative) on Rotor Blade Motion Stability and Flapping”, by Gaffey, Troy, Bell Helicopter Co., Pgs 49 “The Effect of Dynamic Stall on the Response and Airloading of Helicopter Rotor Blades”, by Johnson, Wayne, Massachusetts Institute of Technology, Pgs 68 1969 July 14, 3 “Avionics - Part I Steep Landing Systems for VTOL Aircraft”, by , Pgs 24 “Helicopter Rotor Noise Prediction and Control”, by Schlegel, Ronald, Sikorsky Aircraft Corp., Bausch, William, Pgs 38 1969 October 14, 4 “The ABC Helicopter”, by Cheney, Jr., M. C., United Aircraft Research Laboratories, Pgs 10 “An Analytical Method for Predicting Rotor Wake Geometry”, by Landgrebe, Anton, United Aircraft Research Laboratories, Pgs 20 “Ground and Air Resonance Characteristics of a Soft In-Plane Rigid-Rotor System”, by Donham, R. E., Lockheed-California Co., Cardinale, S. V.; Sachs, I. B., Pgs 33 “Avionics - Part II: Systems Steep Descent Landing Systems for VTOL Aircraft”, by , Pgs 42 “Avionics - Part II: Scanning Beam Landing Systems for VTOL Aircraft”, by Pogust, Frederick B., Airborne Instruments Lab, Pgs 43 1970 January 15, 1 “Flight Simulation of the CH-46 Helicopter”, by Blake, Bruce, The Boeing Co., Albion, Nicholas; Radford, Robert, Pgs 13 “The Influence of Propulsion Systems on Extremely Large Helicopter Design”, by Schneider, J. J., The Boeing Co., Pgs 22 “Fatigue Properties and Test Procedures of Glass Reinforced Plastic Rotor Blades”, by Stepan, Jarosch, Messerschmitt-Bolkow GmbH, Pgs 33 “On the Dynamics of Lifting Rotors With Thrust or Tilting Moment Feedback Controls”, by Johnson, Raymond, US Army, Hohenemser, Kurt, Pgs 42 “Review and Discussion”, by Sissingh, G. J., Lockheed-California Co., Pgs 54 “Helicopter Noise Reduction and Its Effects on Operations”, by Cox, C. R., Bell Helicopter Co., Pgs 59 1970 April 15, 2 “A Self-Monitored Stability Augmentation System for the CX-84 V/STOL Aircraft”, by Griffith, C. D., Canadair, Ltd., Crosby, V. M., Pgs 10 “Convertible Fan/Shaft Engines”, by Seery, Michael E., US Army, Pgs 23 “New Experimental Techniques in Rotorcraft Aerodynamics and Their Application”, by Tanner, W. H., Bell Helicopter Co., Wohlfeld, R. M., Pgs 39 1970 July 15, 3 “Validation of Ground Based Simulation”, by Sinacori, John, Northrop Aircraft Div., Pgs 10 “Measurement and Evaluation of Helicopter Flight Loads Spectra Data”, by Porterfield, John, Kaman Aerospace Corp., Alexander, William, Pgs 22 “Rotor High Speed Performance, Theory vs. Test”, by Harris, Franklin D., The Boeing Co., Tarzanin, Jr., Frank; Fisher, Jr., Richard, Pgs 35 “The Stopped-Rotor Variant of the Proprotor VTOL Aircraft”, by DeTore, J. A., Bell Helicopter Co., Gaffey, T. M., Pgs 45 “Development of VTOL Flying and Handling Qualities Requirements Based on Mission-Task Performance”, by Harper, H. P., Sikorsky Aircraft Corp., Sardanowsky, W.; Scharpf, R., Pgs 57 1970 October 15, 4 “Tail Rotor Design Part II: Structural Dynamics”, by Balke, R., Bell Helicopter Co., Bennett, R. L.; Gaffey, T.; Lynn, R., Pgs 16 “The 'Fenestron,' Shrouded Tail Rotor of the SA. 341 Gazelle”, by Mouille, René, Societe Nationale Industrielle Aerospataiali, Pgs 31 “A Note on a Phenomenon Affecting Helicopter Directional Control in Rearward Flight”, by Huston, Robert, NASA, Morris, Jr., Charles, Pgs 38 “Increasing Tail Rotor Thrust and Comments on Other Yaw Control Devices”, by Robinson, Frank, Hughes Tool Co., Pgs 46
|
