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Fighter Technology Demonstrator Precursor Analysis and Test: Volume II - An Experimental Investigation of the Aerodynamic Characteristics of a Fighter Technology Demonstrator Jet Flap Development Model at Low Subsonic Mach Number
Author(s): Panageas, G. N.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report number: AFFDL TR 73-112 Volume 2
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part III Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design
Author(s): Elsanker, W. K., Okomoto, V. H.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 3
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part II Simulation Studies/Flight Control System Validation
Author(s): Campbell, J. E., Okomuto, V. H., Elsanker, W. K.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 2
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume V Flight Control Technology Part I. Control System Mechanization Trade Studies
Author(s): Phillips, R. W.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 5 Part 1
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume III Performance Methods and Takeoff and Landing Rules
Author(s): Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 3
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume II Design Compendium
Author(s): Roe, M. H., Quam, R. A., et al., Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 2
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STOL Tactical Aircraft Investigation - Externally Blown Flap Volume I Configuration Definition Supplement I Aerodynamic Trades of Flap and Roll Control System
Author(s): Renselaer, D. J.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 1 Supplement 1
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Longitudinal Maneuvering Control Characteristics of a Canard-Wing Fighter Configuration
Author(s): Cichy, Daniel R.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1978-12
Report number: AFFDL TR 78-171 p. 58-87
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An Approach to Simplify the Specification of Low Speed Maneuvering Pitch Control Force
Author(s): Cichy, Daniel R.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1978-12
Report number: AFFDL TR 78-171 p. 300-312
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STOL Tactical Aircraft Investigation - Externally Blown Flap: Volume VI Air Cushion Landing System Trade Study
Author(s): Gustavson, R. G.
Corporate Author(s): Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-04
Report number: AFFDL TR 73-20 Volume 6

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