Fighter planes -- Turbojet enginesSee also what's at your library, or elsewhere.
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Filed under: Fighter planes -- Turbojet engines
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Filed under: Fighter planes- Encyclopedia of US Air Force aircraft and missile systems / : post-World War II fighters (Office of Air Force History : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1978), by Marcelle S Knaack and United States. Air Force. Office of Air Force History (page images at HathiTrust)
- Lightweight fighter aircraft program hearing before a subcommittee of the Committee on Appropriations, United States Senate, Ninety-fourth Congress, first session. (U.S. Govt. Print. Off., 1975), by United States. Congress. Senate. Committee on Appropriations (page images at HathiTrust)
- F-18 Navy air combat fighter hearing before a subcommittee of the Committee on Appropriations, United States Senate, Ninety-fourth Congress, first session, on H.R. 9861 ... : special hearing. (U.S. Govt. Print. Off., 1976), by United States. Congress. Senate. Committee on Appropriations (page images at HathiTrust)
- F-18 program hearings before the Subcommittee on Tactical Airpower of the Committee on Armed Services, United States Senate, Ninety-fourth Congress, first session, September 17 and October 8, 1975. (U.S. Govt. Print. Off., 1976), by United States. Congress. Senate. Committee on Armed Services. Subcommittee on Tactical Air Power (page images at HathiTrust)
- Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Linda S. Bangert, David E. Reubush, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
- Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Francis J. Capone, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
- Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Michael J. Mann, Charles H. Fox, Jarrett K. Huffman, and Langley Research Center (page images at HathiTrust)
- Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Floyd J. Wilcox and Langley Research Center (page images at HathiTrust)
- Theoretical and experimental engine-inlet flow fields for fighter forebodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Steven F. Yaros and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Aga M. Goodsell, John E. Melton, and Ames Research Center (page images at HathiTrust)
- Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by E. Ann Bare, Raymond C. Haddad, David E. Reubush, and Langley Research Center (page images at HathiTrust)
- Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Peter C. Carr, William P. Gilbert, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, and Hugh L. Dryden Flight Research Center (page images at HathiTrust)
- Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 (National Aeronautics and Space Administration ;, 1974), by David E. Reubush, Charles E. Mercer, and Langley Research Center (page images at HathiTrust)
- Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by John W. Paulson, Daniel W. Banks, P. Frank Quinto, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Subsonic and supersonic aerodynamic characteristics of a supersonic cruise fighter model with a twisted and cambered wing with 74 ̊sweep (National Aeronautics and Space Administration ;, 1977), by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effects of stores on longitudinal aerodynamic characteristics of a fighter at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Samuel M. Dollyhigh, William J. Monta, Giuliana Sangiogio, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by James C. Ferris and Langley Research Center (page images at HathiTrust)
- Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Michael J. Mann, Richard L. Campbell, Charles E. Mercer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by David F. Fisher, David M. Richwine, John H. Del Frate, and Dryden Flight Research Facility (page images at HathiTrust)
- Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Michael J. Mann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Francis J. Capone, David E. Reubush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Control definition study for advanced vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Maris Lapins, Grumman Aerospace Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Effect of speed brakes on the supersonic aerodynamic characteristics of a variable-sweep tactical fighter model at Mach numbers from 1.60 to 2.50 (National Aeronautics and Space Administration, 1968), by Celia S. Richardson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 (National Aeronautics and Space Administration ;, 1977), by Richard J. Re, Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5581 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by H. Clyde McLemore, Patricia G. Hemeter, Charles C. Smith, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5409 (National Aeronautics and Space Administration :, 1969), by Joseph R. Chambers, Ernie L. Anglin, James S. Bowman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Subsonic characteristics of a twin-jet swept-wing fighter model with maneuvering devices (National Aeronautics and Space Administration ;, 1973), by Edward J. Ray, Eddie G. Hollingsworth, and Langley Research Center (page images at HathiTrust)
- Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverser (National Aeronautics and Space Administration, 1971), by Donald L. Maiden, Charles E. Mercer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Dynamic stability derivatives of a jet transport configuration with high thrust-weight ratio and an externally blown jet flap (National Aeronautics and Space Administration ;, 1971), by Sue B. Grafton, Charles C. Smith, Lysle P. Parlett, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- NASA TN D-1968 (National Aeronautics and Space Administration, 1963), by Domenic J. Maglieri, John F. Bryant, Virgil S. Ritchie, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Maneuver and buffet characteristics of fighter aircraft (National Aeronautics and Space Administration ;, 1973), by Edward J. Ray, Julian G. Carmichael, Linwood W. McKinney, and Langley Research Center (page images at HathiTrust)
- Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range (National Aeronautics and Space Administration ;, 1973), by Raymond E. Mineck, Myles F. Schwendemann, and Langley Research Center (page images at HathiTrust)
- Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack (National Aeronautics and Space Administration ;, 1974), by Paul L. Coe, William A. Newsom, and Langley Research Center (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryansky, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Harold F. Kleckner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Walter C. Williams, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by S. M. Harmon, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1946), by John A. Zalovcik, Fred L. Daum, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Harry E. Murray, Clarence L. Gillis, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage (National Aeronautics and Space Administration ;, 1974), by Samuel M. Dollyhigh and Langley Research Center (page images at HathiTrust)
- The development of jet-engine Nacelles for a high-speed bomber design (National Advisory Committee for Aeronautics, 1947), by Robert E. Dannenberg, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Tests of submerged duct installation on a modified fighter airplane in the Ames forty by eighty foot wind tunnel. (National Advisory Committee for Aeronautics, 1947), by Norman J. Martin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Experimental investigation of NACA submerged air inlets on a one fifth scale model of a fighter airplane. (National Advisory Committee for Aeronautics, 1947), by Donald E. Gault, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), by Gareth H. Jordan, Stanley P. Butchart, Earl R. Keener, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Spinning and related problems at high angles of attack for high-speed airplanes (National Advisory Committee for Aeronautics, 1956), by Walter J. Klinar, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane (National Advisory Committee for Aeronautics, 1949), by Charles J. Liddell, Donovan R. Heinle, Rudolph D. Van Dyke, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Measurement and analysis of wing and tail buffeting loads on a fighter-type airplane (National Advisory Committee for Aeronautics, 1954), by Wilber B. Huston, T. H. Skopinski, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane (National Aeronautics and Space Administration, 1959), by Gene J. Matranga, Neil Armstrong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers (National Advisory Committee for Aeronautics, 1956), by Charles W. Mathews, Howard C. Kyle, Donald C. Cheatham, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Flight and analytical study of roll requirements of a fighter airplane (National Advisory Committee for Aeronautics, 1956), by James J. Adams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1945), by William N. Turner, Lawrence A. Clousing, Paul J. Steffen, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), by Harold H. Sweberg, Roy H. Lange, Eugene R. Guryanksy, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Tracking performance of a swept-wing figher with a disturbed reticle lead-computing sight (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]., 1955), by Burnett L. Gadeberg, George A. Rathert, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
- Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), by Charles F. Whitcomb, Harry T. Norton, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Defense : acquisition and production of F-15 aircraft : agreement between the United States of America and Japan, effected by exchange of notes signed at Tokyo June 20, 1978. (Dept. of State : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1979), by United States and United States Department of State (page images at HathiTrust)
- Accelerations in fighter-airplane crashes (National Advisory Committee for Aeronautics, 1957), by Loren W. Acker, Jacob C. Moser, Dugald O. Black, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
- Formation lights for fighter aircraft (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Charles A. Baker, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Aerospace Medical Laboratory (U.S.) (page images at HathiTrust)
- A method for predicting three-degree-of-freedom store separation trajectories at speeds up to the critical speed (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1974., 1974), by Frederick K. Goodwin, Marnix F. E. Dillenius, Jack Norman Nielsen, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
- Aerodynamic analysis of a fighter aircraft with a higher order paneling method (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by A. R. Dusto, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Boeing Military Airplane Company (page images at HathiTrust)
- Flight vibration survey of F-106A aircraft (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by H. Kent Reich and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Aircraft motion sensitivity to dynamic stability derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), by T. F. Langham, Inc ARO, United States. Air Force. Arnold Air Force Base, and Arnold Engineering Development Center (page images at HathiTrust)
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