Technical Report Archive & Image Library (TRAIL) - 469 Matching Results

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Primary view of Preliminary Analysis of a Nuclear Powered Supersonic Airplane Using Ramjet Engines
Weber, Richard J. & Connolley, Donald J.
April 11, 1958
Primary view of Hydrogen for Turbojet and Ramjet Powered Flight
Lewis Flight Propulsion Laboratory
April 26, 1957
Primary view of High Altitude Performance Investigation of J65-B-3 Turbojet Engine With Both JP-4 and Gaseous Hydrogen Fuels
Kaufman, Harold R.
April 2, 1957
Primary view of Effect of Combustion Gas Properties on Turbojet-Engine Performance With Hydrogen as Fuel
English, Robert E.
April 10, 1956
Primary view of Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane
Smith, Samuel L., III & Boswinkle, Robert W., Jr.
April 15, 1958
Primary view of Experimental Performance of a 5000-Pound-Thrust Rocket Chamber Using a 20-Percent-Fluorine - 80-Percent-Oxygen Mixture With RP-1
Tomazic, William A.; Kutina, Franklin J., Jr. & Rothenberg, Edward A.
April 24, 1957
Primary view of Combustion of gaseous hydrogen at low pressures in a 35 degree sector of a 28-inch-diameter ramjet combustor
Kerslake, William R.
April 22, 1958
Primary view of Analysis of Flight-Determined and Predicted Effects of Flexibility on the Steady-State Wing Loads of the B-52 Airplane
Kuhl, Albert E.; Rogers, John T. & Little, Mary V.
April 23, 1958
Primary view of Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50
Church, James D.
April 15, 1959
Primary view of Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities
Schmidt, Harold W.
April 17, 1958
Primary view of Full-Scale Wind-Tunnel Tests of a North American FJ-3 Airplane with a Spoiler-Slot-Deflector Lateral Control System
Scallion, William I.
April 9, 1956
Primary view of Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
Phelps, E. Ray
April 20, 1956
Primary view of A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
Phelps, E. Ray & Boyd, John W.
April 30, 1957
Primary view of Wind-Tunnel Investigation at High Subsonic Speeds of the Effects on Static Stability Characteristics of Various Modifications to a Swept-Wing Fighter-Type Airplane Model
Goodson, Kenneth W.
April 30, 1957
Primary view of Analytical Studies of the Response to Longitudinal Control of Three Airplane Configurations in Landing Approaches
Bihrle, William, Jr. & Stone, Ralph W., Jr.
April 9, 1953
Primary view of Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7
Chauvin, Leo T. & Speegle, Katherine C.
April 18, 1957
Primary view of Preliminary Free-Jet Performance of XRJ43-MA-3 Ram-Jet Engine at a Mach Number of 2.70
Welna, Henry J. & Campbell, Carl E.
April 15, 1955
Primary view of Effectiveness of Thermal-Pneumatic Airfoil-Ice-Protection System
Gowan, William H., Jr. & Mulholland, Donald R.
April 13, 1951
Primary view of Flight Investigation to Evaluate the Roll-Rate Stabilization System of the Naval Ordnance Test Station SIDEWINDER Missile at Mach Numbers From 0.9 to 2.3
Brown, Clarence A., Jr. & Nason, Martin L.
April 29, 1954
Primary view of A review of instruments developed for the measurement of the meteorological factors conductive to aircraft icing
Jones, Alun R. & Lewis, William
April 26, 1949
Primary view of Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine
McKann, Robert E. & Petynia, William W.
April 15, 1954
Primary view of Preliminary Wind-Tunnel Investigation of the Effect of Area Suction on the Laminar Boundary Layer Over an NACA 64A010 Airfoil
Braslow, Albert L.; Visconti, Fioravante & Burrows, Dale L.
April 26, 1948
Primary view of Investigation of a 1/22-Scale of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel: Static Longitudinal Stability and Control and Performance Characteristics at Transonic Speeds
Luoma, Arvo A.
April 26, 1956
Primary view of Preliminary Transonic Flutter Investigation of Models of T-Tall of Blackburn NA-39 Airplane
Jones, George W., Jr. & Boswinkle, Robert W., Jr.
April 15, 1958
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