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Primary view of Investigation at Mach Number 1.62 of the Pressure Distribution Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap
Czarnecki, K. R. & Mueller, James N.
January 25, 1950
Primary view of The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings With 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
Strass, H. Kurt
April 25, 1950
Primary view of Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis
Fisher, Lloyd J.
April 25, 1950
Primary view of Model ditching investigations of three airplanes equipped with hydro-skis
Fisher, Lloyd J.
April 25, 1950
Primary view of Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
Acker, Loren W. & Kleinknecht, Kenneth S.
May 25, 1950
Primary view of Determination by the Free-Fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds
Kraft, Christopher C., Jr. & Mathews, Charles W.
August 25, 1950
Primary view of A theoretical investigation of the influence of auxiliary damping in pitch on the dynamic characteristics of a proportionally controlled supersonic canard missile configuration
Nelson, Walter C. & Passera, Anthony L.
August 25, 1950
Primary view of Wing-flow measurements of longitudinal stability and control characteristics of a canard airplane configuration with a 45 degree sweptback wing and a triangular all-movable control surface
Crane, Harold L. & Adams, James J.
August 25, 1950
Primary view of Measurements of Aerodynamic Characteristics of a 35 Degree Sweepback NACA 65-009 Airfoil Model With 1/4 Chord Flap Having 31 Percent Flap Chord Overhang Balance by the NACA Wing Flow Method
Johnson, Harold I. & Goodman, Harold R.
September 25, 1950
Primary view of Comparison of large scale flight measurements of zero lift drag at Mach numbers from 0.9 to 1.7 of two wing-body combinations having similar 60 degree triangular wings with NACA 65A003 sections
Schult, Eugene D.
October 25, 1950
Primary view of Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series
Goodman, Irving A. & Wise, Paul H.
January 25, 1951
Primary view of Preliminary Data on the Effect of Body-Nose Bluntness on the Drag and Pressure Recovery of a Side-Inlet-Body Combination at Mach Numbers of 1.4 and 1.7
Stroud, John F. & Anderson, Warren E.
April 25, 1951
Primary view of Investigation of annular liquid flow with concurrent air flow in horizontal tubes
Kinney, George R. & Abramson, Andrew E.
May 25, 1951
Primary view of Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature
DiPiazza, James T.
May 25, 1951
Primary view of Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
Brajnikoff, George B. & Rogers, Arthur W.
June 25, 1951
Primary view of Comparison of Zero-Lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percent Semispan of a 45 Degrees Sweptback Wing and Body Combination
Hoffman, Sherwood
June 25, 1951
Primary view of Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
Sadoff, Melvin; Roden, William S. & Eggleston, John M.
June 25, 1951
Primary view of Investigation in the Ames 12-Foot Pressure Wind Tunnel of a Model Horizontal Tail of Aspect Ratio 3 and Taper Ratio 0.5 Having the Quarter-Chord Line Swept Back 45 Degrees
Kolbe, Carl D. & Bandettini, Angelo
June 25, 1951
Primary view of Lift and drag coefficients for the Bell X-1 airplane (8-percent-thick wing) in power-off transonic flight
Carman, L. Robert & Carden, John R.
June 25, 1951
Primary view of Pressure-distribution measurements over a 45 degree sweptback wing at transonic speeds by the NACA wing-flow method
Danforth, Edward C. B. & O'Bryan, Thomas C.
June 25, 1951
Primary view of Design of two-dimensional channels with prescribed velocity distributions along the channel walls
Stanitz, John D.
July 25, 1951
Primary view of Flight Investigation of the Drag of Round-Nosed Bodies of Revolution at Mach Numbers From 0.6 to 1.5 Using Rocket-Propelled Test Vehicles
Hart, Roger G.
July 25, 1951
Primary view of A flight study of requirements for satisfactory lateral oscillatory characteristics of fighter aircraft
Liddell, Charles J., Jr.; Creer, Brent Y. & Van Dyke, Rudolph D., Jr.
July 25, 1951
Primary view of A comparison of the calculated maximum-maneuver response characteristics of three air-to-air, beam-rider, guided missiles having different lift ratios
Matthews, Howard F. & Stewart, Elwood C.
September 25, 1951
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