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Parametric Performance Analysis Of Crew Escape Concepts In The Vtol And Conventional Take-Off And Landing Situations
Author(s): Brown, Dean W., Standish, David B.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-01
Report number: AFFDL TR 67-178
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Propulsion System Flow Stability Program (Dynamic). Part XII. Unsteady Combustion in Duct Burners and Afterburners
Author(s): Dix, D. M., Duffield, P. L., Smith, J. E.
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 XII
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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 Allowables for Titanium Alloys
Author(s): Martin, Gardner R., Sommer, Alfred W.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-06
Report number: AFML TR 69-161
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Propulsion System Integration and Test Program (Steady State). Part II. Shared Exit Ejector Nozzle Static Tests
Author(s): Alfano, David L.
Corporate Author(s): North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1969-06
Report number: AFAPL TR 69-44 Part 02