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Propulsion System Flow Stability Program (Dynamic). Part XVI. Survey of Sensors Applicable to the Control of Aircraft Propulsion Systems
Author(s): Wolfshagen, Ronald G., Ogura, Isaac A.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1968-12
Report number: AFAPL TR 68-142 Part XVI
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Propulsion System Flow Stability Program (Dynamic). Part XVII. Propulsion System Simulation Digital Computer Program Format and Routines
Author(s): Kaplan, Earl H., Wong, Heeman W.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1968-12
Report number: AFAPL TR 68-142 Part XVII
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Propulsion System Flow Stability Program (Dynamic). Part XX. Computer Programs for the Root Locus Analysis of Linearized Turbojet and Turbofan Control Systems
Author(s): Lum, Evan L.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1968-12
Report number: AFAPL TR 68-142 Part XX
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part I, General And Summary Information
Author(s): McClure, James G., Shumway, Justin F., Cragin, Glen P., Jr
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-31 Part 1
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part II. Shakedown Testing In Vad 7-Ft X 10-Ft Low Speed Wind Tunnel
Author(s): Meyer, Robert D., English, Robert B., Davidson, Jim K.
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-31 Part 2
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part III, Testing In 17 Ft Test Section Of 7 Ft X 10 Ft Wind Tunnel, Nasa Langley Research Center
Author(s): Brownrigg, William E., Jr., English, Robert B., Meyer, Robert D.
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-31 Part 3
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Design, Fabrication, Testing, And Data Analysis Of Adam II Concept (Propulsive Wing). Part IV. Testing In The Langley Research Center 16-Foot Transonic Wind Tunnel
Author(s): English, Robert B., Davidson, Jim K., Brownrigg, William E., Jr.
Corporate Author(s): LTV Aerospace Corp Dallas Tx Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-31 Part 4
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Large Deflection And Stability Analysis Of Two-Dimensional Truss And Frame Structures
Author(s): Przemieniecki, John S., Purdy, David M.
Corporate Author(s): Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-38
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Evaluation And Utilization Of Airplane Flight Loads Data. Part I. Techniques And Uncertainities
Author(s): Gray, Cory L.
Corporate Author(s): Measurement Analysis Corp Los Angeles CA
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-52 Part 1
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Evaluation And Utilization Of Airplane Flight Loads Data. Part II. Data Acquisition Equipment Performance And Accuracy
Author(s): Rentz, Peter E.
Corporate Author(s): Measurement Analysis Corp Los Angeles CA
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-05
Report number: AFFDL TR 68-52 Part 2

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