The Online Books Page

Fighter planes

See also what's at Wikipedia, your library, or elsewhere.

Broader term:

Airplanes, Military

Narrower terms:

Used for:

Fighters (Airplanes)
Pursuit planes
Fighter-bombers

Filed under: Fighter planes

Aircraft development : the Advanced Tactical Fighter's costs, schedule, and performance goals : report to the Chairman, Committee on Armed Services, House of Representatives / (Washington, DC : The Office, 1988), by United States General Accounting Office and United States House Committee on Armed Services (page images at HathiTrust)
Tactical fighter aircraft : differences between the Air Force's roadmap and the Five Year Defense Plan : report to the Chairman, Committee on Armed Services, House of Representatives / (Washington, D.C. The Office, 1990), by United States General Accounting Office (page images at HathiTrust)
Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot-deflector controls on an unswept-wing fighter-type airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Dewey E. Wornom and Langley Research Center (page images at HathiTrust)
HIgh acceleration cockpit controller locations / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975), by Air Force Flight Dynamics Laboratory (U.S.) and McDonnell Aircraft Company (page images at HathiTrust)
Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,), by Linda S. Bangert, David E. Reubush, Laurence D. Leavitt, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Floyd J. Wilcox and Langley Research Center (page images at HathiTrust)
Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : for sale by the National Technical Information Service], 1979), by John W. Paulson, James L. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Infrmation Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by David E. Reubush, Charles E. Mercer, and Langley Research Center (page images at HathiTrust)
Subsonic maneuver capability of a supersonic cruise fighter wing concept / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Gregory D. Riebe, Charles H. Fox, and Langley Research Center (page images at HathiTrust)
Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Michael J. Mann, Charles E. Mercer, and Langley Research Center (page images at HathiTrust)
Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Jack Nugent, Odis C. Pendergraft, and Ames Research Center (page images at HathiTrust)
Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at mach 1.60 to 2.87 / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by M. Leroy Spearman, William J. Monta, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Daniel G. Murri, Sue B. Grafton, Luat T. Nguyen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1981), by William P. Henderson, Laurence D. Leavitt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Operational performance of vapor-screen systems for in-flight visualization of leading-edge vortices on the F-106B aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by John E. Lamar (page images at HathiTrust)
Effects of stores on longitudinal aerodynamic characteristics of a fighter at supersonic speeds / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by David E. Hahne and Langley Research Center (page images at HathiTrust)
An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Francis J. Capone, Laurence D. Leavitt, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by James C. Ferris and Langley Research Center (page images at HathiTrust)
Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Jay M. Brandon and Langley Research Center (page images at HathiTrust)
Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Sue B. Grafton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Michael J. Mann and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Frank J. Kurtenbach, Frank W. Burcham, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Laurence D. Leavitt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Laurence D. Leavitt, E. Ann Bare, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Control definition study for advanced vehicles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Warren F. Ahtye and Ames Research Center (page images at HathiTrust)
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 / (Washington, D.C. : 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)
A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Kenneth C. Weston, Joanna E. Swanson, and United States. National Aeronautics and Space Administration. Space Task Group (page images at HathiTrust)
Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverser / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett, Homer G. Morgan, A. Gerald Rainey, and Langley Research Center (page images at HathiTrust)
Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane / (Washington D.C. : National Aeronautics and Space Administration, 1959), by William F. Hinson and Langley Research Center (page images at HathiTrust)
An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Lowell E. Hasel and Langley Research Center (page images at HathiTrust)
Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Charles B. Rumsey, Dorothy B. Lee, and Langley Research Center (page images at HathiTrust)
Wave drag as the objective function in transonic fighter wing optimization / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Pamela S. Phillips and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Wing planform effects at supersonic speeds for an advanced fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by National Technical Information Service], 1984), by Richard M. Wood, D. S. Miller, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Theoretical and experimental engine-inlet flow fields for fighter forebodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Steven F. Yaros and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Michael J. Mann, James C. Ferris, Richard L. Campbell, 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 / (Washington, D.C. : 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 / (Washington, D.C. : 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)
Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Samuel M. Dollyhigh, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Francis J. Capone, Bobby L. Berrier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Dale R. Satran, Ernie L. Anglin, William P. Gilbert, and Langley Research Center (page images at HathiTrust)
Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Richard M. Wood, D. S. Miller, 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Odell A. Morris and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Subsonic and supersonic longitudinal stability and control characteristics of an aft-tail fighter configuration with cambered and uncambered wings and cambered fuselage / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Samuel M. Dollyhigh 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Richard J. Re, Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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)
R.A.F. log book [electronic resource]. ([London? : Ministry of Information, 1943?]), by Great Britain. Ministry of Information (page images at HathiTrust)
SAC's fighter planes and their operations / (Offutt AFB, NE : Office of the Historian, Headquarters Strategic Air Command ; Washington, D.C. : For sale by the Supt. of Docs, U.S. G.P.O., [1988]), by Robert J. Boyd (page images at HathiTrust)
Post-World War II fighters, 1945-1973 / (Washington, D.C. : Office of Air Force History, U.S. Air Force, 1985), by Marcelle Size Knaack (page images at HathiTrust)
Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Jack Nugent and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Pilot training manual for the Black Widow, P-61, prepared for Headquarters, AAF, Office of Assistant Chief of Air Staff Training. ([Washington, 1944?]), by United States. Army Air Forces. Office of Flying Safety and Training United States. Army Air Forces. Office of Assistant Chief of Air Staff (page images at HathiTrust)
Alternatives for modernizing U.S. fighter forces. (Washington, D.C. : Congressional Budget Office : For sale by the Supt. of Docs., U.S. G.P.O., [2009]), by David Arthur, Kevin Eveker, and United States Congressional Budget Office (page images at HathiTrust)
Strategies for maintaining the Navy's and Marine Corps' inventories of fighter aircraft. ([Washington, D.C.] : Congress of the U.S., Congressional Budget Office, [2010]), by United States Congressional Budget Office (page images at HathiTrust)
Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Frederick L. Moore, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Encyclopedia of US Air Force aircraft and missile systems / : post-World War II fighters / (Washington : Office of Air Force History : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1978-<1988 >), by Marcelle S Knaack and United States. Air Force. Office of Air Force History (page images at HathiTrust)
Joint strike fighter acquisition reform : will it fly? : hearing before the Subcommittee on National Security, Veterans Affairs, and International Relations of the Committee on Government Reform, House of Representatives, One Hundred Sixth Congress, second session, May 10, 2000. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., [Congressional Sales Office], 2001), by Veterans Affairs United States. Congress. House. Committee on Government Reform. Subcommittee on National Security (page images at HathiTrust)
F-18 Navy air combat fighter [microform] : hearing before a subcommittee of the Committee on Appropriations, United States Senate, Ninety-fourth Congress, first session, on H.R. 9861 ... : special hearing. (Washington : U.S. Govt. Print. Off., 1975), by United States. Congress. Senate. Committee on Appropriations (page images at HathiTrust)
F-18 program [microform] : 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. (Washington : U.S. Govt. Print. Off., 1976), by United States. Congress. Senate. Committee on Armed Services. Subcommittee on Tactical Air Power (page images at HathiTrust)
Lightweight fighter aircraft program [microform] : hearing before a subcommittee of the Committee on Appropriations, United States Senate, Ninety-fourth Congress, first session. (Washington : U.S. Govt. Print. Off., 1975), by United States. Congress. Senate. Committee on Appropriations (page images at HathiTrust)
Sierra Hotel : flying Air Force fighters in the decade after Vietnam / (Washington, D.C. : Air Force History and Museums Program, U.S. Air Force : [Supt. of Docs., U.S. G.P.O., distributor], 2001), by C. R. Anderegg and Air Force History and Museums Program (U.S.) (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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Samuel M. Dollyhigh and Langley Research Center (page images at HathiTrust)
The ace factor : air combat & the role of situational awareness / (Annapolis, Md. : Naval Institute Press, 1988), by Mike Spick (page images at HathiTrust)
The history of Naval Air Station, Patuxent River, Maryland. (Patuxent River, Md. : The Station, [1999]), by Linda Drew and Naval Air Station Patuxent River (Md.) (page images at HathiTrust)
Proposed joint development of the FSX fighter with Japan : hearings before the Subcommittee on Economic Stabilization of the Committee on Banking, Finance, and Urban Affairs, House of Representatives, One Hundred First Congress, first session, April 18 and May 5, 1989. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1989), by Finance United States. Congress. House. Committee on Banking (page images at HathiTrust)
DOD Inspector General's report on Defense Acquisition Board review of F/A-18 E/F aircraft : joint hearing before the Procurement and Military Nuclear Systems Subcommittee and the Research and Development Subcommittee of the Committee on Armed Services, House of Representatives, One Hundred Second Congress, second session, hearing held June 30, 1992. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1993), by United States. Congress. House. Committee on Armed Services. Procurement and Military Nuclear Systems Subcommittee and United States. Congress. House. Committee on Armed Services. Subcommittee on Research and Development (page images at HathiTrust)
Hearing on National Defense Authorization Act for Fiscal Year 2009 and oversight of previously authorized programs before the Committee on Armed Services, House of Representatives, One Hundred Tenth Congress, second session : Air and Land Forces Subcommittee meeting jointly with the Seapower and Expeditionary Forces Subcommittee on budget request on Departments of the Navy and Air Force tactical aviation programs, hearing held, March 11, 2008. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., 2008), by United States. Congress. House. Committee on Armed Services. Subcommittee on Air and Land Forces and United States. Congress. House. Committee on Armed Services. Seapower and Expeditionary Forces Subcommittee (page images at HathiTrust)
The sale of F-5E/F aircraft to Honduras : hearing and markup before the Committee on Foreign Affairs and its subcommittees on Arms Control, International Security, and Science and on Western Hemisphere Affairs, House of Representatives, One hundredth Congress, first session ... May 19 and June 4, 1987. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1987), by United States House Committee on Foreign Affairs, United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Western Hemisphere Affairs, and International Security United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Arms Control (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. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 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)
Tracking performance of a swept-wing figher with a disturbed reticle lead-computing sight /, 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 /, by Charles F. Whitcomb, Harry T. Norton, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Is DOD meeting Joint Strike Fighter (JSF) international cooperative program goals? : hearing before the Subcommittee on National Security, Emerging Threats and International Relations of the Committee on Government Reform, House of Representatives, One Hundred Eighth Congress, first session, July 21, 2003. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., [Congressional Sales Office], 2004), by Emerging Threats United States. Congress. House. Committee on Government Reform. Subcommittee on National Security (page images at HathiTrust)
Hearing on National Defense Authorization Act for fiscal year 2010 and oversight of previously authorized programs before the Committee on Armed Services, House of Representatives, One Hundred Eleventh Congress, first session : Air and Land Forces Subcommittee hearing on budget request for Air Force modernization programs, hearing held, May 20, 2009. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., 2009), by United States. Congress. House. Committee on Armed Services. Subcommittee on Air and Land Forces (page images at HathiTrust)
The F-22 program : hearing before the Air and Land Forces Subcommittee of the Committee on Armed Services, House of Representatives, One Hundred Tenth Congress, second session, hearing held, November 19, 2008. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., 2010), by United States. Congress. House. Committee on Armed Services. Subcommittee on Air and Land Forces (page images at HathiTrust)
Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane / (Langley Field, VA : 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)
Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high mach numbers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold F. Kleckner, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
An approximate determination of the power required to move control surfaces as related to control-booster design / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight tests of the lateral control characteristics of an F6F-3 airplane equipped with spring-tab ailerons / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Walter C. Williams, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by S. M. Harmon, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Harold I. Johnson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Flight studies of the horizontal-tail loads experienced by a modern pursuit airplane in abrupt maneuvers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Langley Aeronautical Laboratory and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint / (Langley Field, VA : 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)
An automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane / (Langley Field, VA : 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)
Emergency measures for increasing the range of fighter airplanes / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943), by Robert T. Jones, Joseph W. Wetmore, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight / (Washington, D.C. : NACA, 1953), by Norman M. McFadden, Harry A. James, John L. McCloud, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
Generalized hot-gas ingestion investigation of large-scale jet VTOL fighter-type models. (Washington, D.C. : 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)
Approach and landing investigation at lift-drag ratios of 2 to 4 utilizing a straight-wing fighter airplane / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Gene J. Matranga, Neil Armstrong, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Francis J. Capone, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
Analysis of flight data from a high-incidence research model by system identification methods / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by James G. Batterson, Vladislav Klein, and Langley Research Center (page images at HathiTrust)
Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Jack Nugent, Bruce G. Powers, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Edward J. Ray, Eddie G. Hollingsworth, and Langley Research Center (page images at HathiTrust)
Technical notes / (Urbana, Ill. : [s.n.], 1918), by University of Illinois (Urbana-Champaign campus). School of Military Aeronautics (page images at HathiTrust)
Conceptual design optimization study / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by S. J. Hollowell, R. M. Hiyama, E. R. Beeman, Langley Research Center, and North American Aircraft (Firm) (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 / (Washington, D.C. : 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)
Assessing the impact of modeling limits on intelligent systems / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by William B. Rouse, John M. Hammer, Langley Research Center, and Inc Search Technology (page images at HathiTrust)
Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 ̊to 110 (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Sue B. Grafton, Charles E. Libbey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Raymond E. Mineck, Myles F. Schwendemann, and Langley Research Center (page images at HathiTrust)
Maneuver and buffet characteristics of fighter aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Edward J. Ray, Julian G. Carmichael, Linwood W. McKinney, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Paul L. Coe, William A. Newsom, and Langley Research Center (page images at HathiTrust)
Free-flight model investigation of a vertical-attitude VTOL fighter / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by William A. Newsom, Ernie L. Anglin, and Langley Research Center (page images at HathiTrust)
The development of jet-engine Nacelles for a high-speed bomber design / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Robert E. Dannenberg, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Donald E. Gault, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : 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. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Gene J. Matranga, Katharine H. Armistead, Flight Research Center (U.S.), and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
A computer technique for detailed analysis of mission radius and maneuverability characteristics of fighter aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Willard E. Foss, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Norman J. Martin, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
Measurement and analysis of wing and tail buffeting loads on a fighter-type airplane / (Washington, D.C. : 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)
1993 Air Force budget : potential reductions to research, development, test, and evaluation programs : briefing report to Congressional requesters / (Washington, D.C. : The Office ; Gaithersburg, MD (P.O. Box 6015, Gaithersburg 20877) : The Office [distributor, 1992]), by United States General Accounting Office (page images at HathiTrust)
The sale of F-5E/F aircraft to Honduras : hearing and markup before the Committee on Foreign Affairs and its subcommittees on Arms Control, International Security, and Science and on Western Hemisphere Affairs, House of Representatives, One hundredth Congress, first session ... May 19 and June 4, 1987. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1987), by United States House Committee on Foreign Affairs, United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Western Hemisphere Affairs, and International Security United States. Congress. House. Committee on Foreign Affairs. Subcommittee on Arms Control (page images at HathiTrust)
Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane / (Washington, D.C. : 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)
A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane / (Washington, D.C. : 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)
A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers / (Washington, D.C. : 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)
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. ([Washington] : Dept. of State : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1978), by etc. Japan United States. Treaties and United States Department of State (page images at HathiTrust)
The Joint Strike Fighter : hearing before the Committee on Armed Services, United States Senate, One Hundred Eleventh Congress, second session, March 11, 2010 (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., 2011), by United States Senate Committee on Armed Services (page images at HathiTrust)
Accelerations in fighter-airplane crashes / (Washington, D.C. : 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)
U.S.-Japan codevelopment : review of the FS-X program : briefing report to Congressional requesters / ([Washington, D.C.] : The Office, 1990), by United States General Accounting Office (page images at HathiTrust)
Tactical aircraft programs : hearing before the Military Research and Development Subcommittee, joint with Military Procurement Subcommittee, of the Committee on National Security, House of Representatives, One Hundred Fourth Congress, second session, hearing held June 27, 1996. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1997), by United States. Congress. House. Committee on National Security. Subcommittee on Military Research and Development and United States. Congress. House. Committee on National Security. Subcommittee on Military Procurement (page images at HathiTrust)
F-22 pilot physiological issues : hearing before the Subcommittee on Tactical Air and Land Forces of the Committee on Armed Services, House of Representatives, One Hundred Twelfth Congress, second session, hearing held September 12, 2012., by United States. Congress. House. Committee on Armed Services. Tactical Air and Land Forces Subcommittee (page images at HathiTrust)
Navy, Marine Corps, and Air Force tactical aviation programs : hearing before the Subcommittee on Tactical Air and Land Forces of the Committee on Armed Services, House of Representatives, One Hundred Twelfth Congress, first session, hearing held March 15, 2011. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., U.S. G.P.O., 2011), by United States. Congress. House. Committee on Armed Services. Tactical Air and Land Forces Subcommittee (page images at HathiTrust)
Spinning and related problems at high angles of attack for high-speed airplanes / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Walter J. Klinar, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight and analytical study of roll requirements of a fighter airplane / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by James J. Adams and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1957]), by S. A. Sjoberg, William L. Alford, Walter R. Russell, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
CVAN-70 aircraft carrier : joint hearings before the Joint Senate-House Armed Services Subcommittee of the Senate and House Armed Services Committees on ... Ninety-first Congress, second session ... April 7, 8, 10, 13, and 16, 1970. (Washington, U.S. Govt. Print. Off., 1970), by United States. Congress. Joint Senate-House Armed Services Subcommittee on CVAN-70 Aircraft Carrier (page images at HathiTrust)
Aircraft development : Navy's participation in Air Force's Advanced Tactical Fighter program : report to the Chairman, Committee on Armed Services, House of Representatives / (Washington, DC : The Office, 1990), by United States General Accounting Office and United States House Committee on Armed Services (page images at HathiTrust)
Compressibility effects on the longitudinal stability and control of a pursuit-type airplane as measured in flight / (Washington, D.C. : 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)

More items available under narrower terms.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.