F-16 (Jet fighter plane)See also what's at Wikipedia, your library, or elsewhere.
Broader term:Narrower terms:Used for:- F-16 (Fighter planes)
- General Dynamics F-16 Fighting Falcon
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Filed under: F-16 (Jet fighter plane)- Proposed sale of F-16 aircraft and weapons systems of [i.e. to] Pakistan : hearing before the Committee on International Relations, House of Representatives, One Hundred Ninth Congress, second session, July 20, 2006. (U.S. G.P.O. :, 2006), by United States House Committee on International Relations (page images at HathiTrust)
- Defeating al-Qaeda's air force : Pakistan's F-16 program in the fight against terrorism : hearing before the Subcommittee on the Middle East and South Asia of the Committee on Foreign Affairs, House of Representatives, One Hundred Tenth Congress, second session, September 16, 2008. (U.S. G.P.O. :, 2008), by United States. Congress. House. Committee on Foreign Affairs. Subcommittee on the Middle East and South Asia (page images at HathiTrust)
- Korean fighter program : joint hearing before the Subcommittees on Arms Control, International Security, and Science and Asian and Pacific Affairs of the Committee on Foreign Affairs, House of Representatives, One Hundred Second Congress, first session, August 1, 1991. (U.S. G.P.O. :, 1992), by International Security United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Arms Control and United States House Subcommittee on Asian and Pacific Affairs (page images at HathiTrust)
- The proposed sale of F-16ʼs to Pakistan : hearing before the Subcommittee on Arms Control, International Security, and Science, and on Asian and Pacific Affairs of the Committee on Foreign Affairs, House of Representatives, One Hundred First Congress, first session, August 2, 1989. (U.S. G.P.O. :, 1989), by International Security United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Arms Control and United States House Subcommittee on Asian and Pacific Affairs (page images at HathiTrust)
- Review of administration's policy on sales of advanced fighter planes to ASEAN : hearing before the Subcommittees on International Security and Scientific Affairs and on Asian and Pacific Affairs of the Committee on Foreign Affairs, House of Representatives, Ninety-eighth Congress, second session, March 28, 1984. (U.S. G.P.O., 1984), by United States. Congress. House. Committee on Foreign Affairs. Subcommittee on International Security and Scientific Affairs and United States House Subcommittee on Asian and Pacific Affairs (page images at HathiTrust)
- United States-Japanese security cooperation and the FSX agreement : hearings and markup before the Committee on Foreign Affairs and its Subcommittees on Arms Control, International Security, and Science, on Asian and Pacific Affairs, and on International Economic Policy and Trade, House of Representatives, One Hundred First Congress, first session, on S.J. Res. 113, April 13, May 3, 9, 10, 18, and 23, 1989. (U.S. G.P.O. :, 1989), by International Security United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Arms Control, United State House Subcommittee on International Economic Policy and Trade, and United States House Subcommittee on Asian and Pacific Affairs (page images at HathiTrust)
- AID and the proposed arms sales of F-16's to Pakistan : hearings before the Committee on Foreign Relations, United States Senate, Ninety-seventh Congress, first session, November 12 and 17, 1981. (U.S. G.P.O., 1982), by United States Senate Committee on Foreign Relations (page images at HathiTrust)
- Proposed sale of F-16's to Venezuela : hearing before the Committee on Foreign Relations, United States Senate, Ninety-seventh Congress, second session, February 5, 1982. (U.S. G.P.O., 1982), by United States Senate Committee on Foreign Relations (page images at HathiTrust)
- Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Luat T. Nguyen, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Ground vibration test of F-16 airplane with initial decoupler pylon (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by F. W. Cazier, M. W. Kehoe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- The multinational F-16 aircraft program : its progress and concerns : report to the Congress (U.S. General Accounting Office], 1979), by United States General Accounting Office (page images at HathiTrust)
- Why Taiwan matters : hearing before the Committee on Foreign Affairs, House of Representatives, One Hundred Twelfth Congress, first session. (U.S. G.P.O. :, 2011), by United States House Committee on Foreign Affairs (page images at HathiTrust)
- Reduced order model based feedback control of large-scale aeroelastic simulations (Arlington, Virginia. : Air Force Office of Scientific Research, 2008., 2008), by M. J. Balas, Casey Fagley, University of Wyoming. Department of Electrical and Computer Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
- Documentation of a transonic wind tunnel test to investigate the separation characteriscis of the GBU-10C/B, the CBU-58, and the BL-755 stores from the F-16 aircraft (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by J. M. Wright, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), by Earl A. Price, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Filed under: F-16 (Jet fighter plane) -- CostsFiled under: F-16 (Jet fighter plane) -- Design and constructionFiled under: F-16 (Jet fighter plane) -- Testing
Items below (if any) are from related and broader terms.
Filed under: Jet fighter planes- A free-flight investigation of the drag coefficients of two single-engine supersonic interceptor configurations from Mach number 0.8 to 1.90 to determine the effect of inlet and engine locations (National Advisory Committee for Aeronautics, 1955), by Joseph H. Judd, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Acoustic environments of the F-111A aircraft during ground runup (Wright-Patterson Air Force Base, Ohio : Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1968., 1968), by John N. Cole, Justus F. Rose, and Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
- Flight investigation of fighter side-stick force-deflection characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975., 1975), by G. Warren Hall, Rogers E. Smith, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Aircraft motion sensitivity to cross and cross-coupling damping derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by R. W. Butler, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Afterbody drag investigation of a twin-nozzle fighter-type model at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), by Earl A. Price, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Filed under: Jet fighter planes -- Computer programs- Integrated airframe - nozzle performance for designing twin-engine fighters. Volume VI, Revised operating manual for twin nozzle/afterbody drag and nozzle internal performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Evaluation of the twin nozzle/afterbody drag and nozzle internal performance computer deck with ESIT free jet data (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, 1974., 1974), by Phillip C. Everling, Douglas L. Bowers, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Integrated airframe - nozzle performance for designing twin-engine fighters. Volume V, Operating manual for supersonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Integrated airframe - nozzle performance for designing twin-engine fighters. Volume IV, Operating manual for subsonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
Filed under: Jet fighter planes -- Design and construction- Integrated airframe - nozzle performance for designing twin-engine fighters. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Analysis/Theory of controlled configured structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by J. G. Williams, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)
- Flight propulsion control coupling for thrust vectoring fighter aircraft. Volume III, Phase II (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980., 1980), by Frederick C. Glaser, Douglas Aircraft Company, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Filed under: Jet fighter planes -- Testing- Buffet characteristics of the model F-4 airplane in the transonic flight regime (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1970., 1970), by Marshall Cohen, Air Force Flight Dynamics Laboratory (U.S.), McDonnell Aircraft Company, and United States. Air Force. Systems Command (page images at HathiTrust)
- Final test report : X-29A Vortex Flow Control (VFC) flight test results (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), by Frank Luria, Brian Hobbs, Paul Pellicano, Joseph Krumenacker, William Gillard, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
Filed under: Jet fighter planes -- Wind tunnel testing- Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 (National Aeronautics and Space Administration, 1961), by Robert P. Smith, William C. Moseley, and United States. National Aeronautics and Space Administration. Space Task Group (page images at HathiTrust)
- Low-speed measurements of oscillatory lateral stability derivatives of a model of 60 degree delta-wing bomber (National Aeronautics and Space Administration, 1959), by John W. Paulson and Langley Research Center (page images at HathiTrust)
- Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M equals 4 (National Aeronautics and Space Administration, 1959), by Barbara J. Sort, Simon C. Sommer, and Ames Research Center (page images at HathiTrust)
- Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing (National Aeronautics and Space Administration, 1959), by Earl R. Keener and Flight Research Center (U.S.) (page images at HathiTrust)
- Research on blunt-faced entry configurations at angles of attack Between 60° and 90° (National Aeronautics and Space Administration, 1960), by William H. Phillips and Langley Research Center (page images at HathiTrust)
- Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75 degree and 108 degree (National Aeronautics and Space Administration, 1960), by Ross B. Robinson, Paul W. Howard, and Langley Research Center (page images at HathiTrust)
- Wind-tunnel investigation of Saturn S-IC AERODYNAMIC engine gimbal forces and base pressures using a cold-flow-jet simulation technique (National Aeronautics and Space Administration ;, 1967), by Bernard J. Blaha, Donald L. Bresnahan, Robert A. Wasko, and Lewis Research Center (page images at HathiTrust)
- Effects of 3 spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45 degree sweptback highly tapered wing at transonic speeds (National Aeronautics and Space Administration, 1959), by John P. Mugler and Langley Research Center (page images at HathiTrust)
- Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings (National Aeronautics and Space Administration, 1960), by Bernard Spencer and Langley Research Center (page images at HathiTrust)
- The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack (National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, William J. Alford, A. Warner Robins, and Langley Research Center (page images at HathiTrust)
- Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster (National Aeronautics and Space Administration, 1960), by Albin O. Pearson and Langley Research Center (page images at HathiTrust)
- Integrated airframe - nozzle performance for designing twin-engine fighters. Volume II, Wind tunnel data identification and presentation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by Edsel R. Glasgow, T. J. Jones, D. A. Tappeiner, T. E. Charbonneau, D. K. Hill, R. D. Grennan, R. A. Fox, D. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
- Wind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by J. C. Donaldson, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Pressure test of three elliptic missile body configuratins (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1985., 1985), by Marvin E. Sellers, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
- Aerodynamic characteristics and store loads of a 1/24-scale F-111 aircraft model with three external store loadings (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), by C. F. Anderson, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
- An Experimental study of several wind tunnel wall configurations using two V/STOL model configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), by T. W. Binion, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Use of the flow angularity technique for predicting store separation trajectories (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Product Assurance Division, Air Force Systems Command, United States Air Force, 1971., 1971), by Stephen C. Korn, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
- A Wind tunnel test to study the mutual interference of multiple bodies in the flow field of the F-4C aircraft in the transonic speed range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), by A. A. Hesketh, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
- Validation and expansion of the flow angularity technique for predicting store separation trajectories (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aircraft Compatibility and Weapons Flight Dynamics Branch, Product Assurance Division, Air Force Systems Command, United States Air Force, 1972., 1972), by Stephen C. Korn, United States. Air Force. Systems Command, and Air Force Armament Laboratory (page images at HathiTrust)
- Pressure and static force test of three elliptic missile body configurations at mach numbers 1.5 to 5.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), by M. E. Sellers, L Siler, Air Force Wright Aeronautical Laboratories, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
- Static stability test of three elliptic missile body configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1985., 1985), by Marvin E. Sellers, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
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