- NASA TN D-3845 Rolling stability derivatives of a variable-sweep tactical fighter model at subsonic speeds
William P. Henderson/ W. Pelham Phillips and Thomas G.Gainer
February 1967 - NASA TN D-6490 Comparison of in-flight F-111A inlet performance for on and off-scheduled inlet geometry at mach numbers of 0.68 to 2.18
Richard A. Martin and Donald L. Hughes
September 1971 - NASA TM X-2759 A Wind-tunnel investigation of the NASA supercritical airfoil to a variable-wing-sweep fighter airplane
Theodore G. Ayers
July 1973 - NASA TM X-3095 Wind-tunnel investigation of aerodynamic load distribution on a variable-wing-sweep fighter airplane with a NASA supercritical airfoil
J.B. Hallissy and C. D Harris
October 01 1974 - NASA TP 1368 Flight Comparison of the Transonic Agility of the F-111A Airplane and the F-111 Supercritical Wing Airplane
Edward L. Friend and Glenn M. Sakamoto
December 1978 - NASA TM 88267 AFTI/F-111 MAX Flight control system and Redundancy Management Description
Richard R. Larson
February 1987 - AEDC-TSR-79-P27 Wind tunnel test to investigate aerodynamic hysteresis phenomena of the F-4 and F-111 aircraft models
Joseph F. Herman
May 15 1979 - AEDC-TR-78-35 / AFATL-TR-78-55 Aerodynamic characteristics of a 1/24 scale F-111 aircraft with various external stores at mach numbers from 0.5 to 1.3
C. F. Anderson
July 1978 - AEDC-TR-78-35 / AFATL-TR-78-55 Aerodynamic characteristics of a 1/24 scale F-111 aircraft with various external stores at mach numbers from 0.5 to 1.3
C. F. Anderson
July 1978 - DSTO-TR-0321 F-111C Longitudinal and Lateral aerodynamic flight data analysis for take-off and landing configurations
Andrew D. Snowden and Jan S. Drobik
April 1996 - NASA TN D-7376 Investigation of coaxial jet noise and inlet choking using an F-111A airplane
Terrill W. Putname
August 1972 - NASA CR-152114 An investigation of wing buffeting response at subsonic and transonic speeds Phase II F-111A Flight Data Analysis Volume II Tabulated Power Spectra
David B. Benepe/ Atlee M. Cunningham Jr/ Sam Traylor Jr./ W. David Dunmyer
1978
TF30 engines data
- NASA TM X-3106 REAL-TIME SIMULATION OF THE TF30-P-3 TURBOFAN ENGINE USING A HYBRID COMPUTER, John R. Szuch and William N. Bruton, Lewis Research Center, October 1974
W. H. Davis - NASA CR-134996, MODELING AND ANALYSIS OF THE TF30-P-3 COMPRESSOR SYSTEM WITH INLET PRESSURE DISTORTION, R. S. Mazzawy and G. A. Banks, Pratty & Whitney Aircraft, April 1976
W. H. Davis