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Primary view of Aerodynamic Heating of Blunt Nose Shapes at Mach Numbers Up to 14
Stoney, William E., Jr.
August 11, 1958
Primary view of Aerodynamic heating of blunt nose shapes at Mach numbers up to 14
Stoney, William E., Jr.
August 11, 1958
Primary view of Flight, Analog-Simulator, and Analytical Studies of an Automatically Controlled Interceptor Which Uses a Bank-Angle-Error Computer for Lateral Commands
Cheatham, Donald C. & Brissenden, Roy F.
August 11, 1958
Primary view of Stability of Ballistic Reentry Bodies
Bird, John D. & Reese, David E., Jr.
August 11, 1958
Primary view of The static longitudinal characteristics of a twisted and cambered 45 degree sweptback wing at Mach numbers up to 0.96
Sammonds, Robert I. & Reynolds, Robert M.
August 11, 1958
Primary view of Effect of Dissociation on Exhaust-Nozzle Performance
Reynolds, T. W.
June 11, 1958
Primary view of Effect of Dissociation on Exhaust-Nozzle Performance
Reynolds, T. W.
June 11, 1958
Primary view of Effect of pressure level on afterburner-wall temperatures
Shillito, Thomas B. & Smolak, George R.
June 11, 1958
Primary view of Effect of pressure level on afterburner-wall temperatures
Shillito, Thomas B. & Smolak, George R.
June 11, 1958
Primary view of Performance of JP-4 Fuel With Fluorine-Oxygen Mixtures in 1000-Pound-Thrust Rocket Engines
Nored, Donald L. & Douglass, Howard W.
June 11, 1958
Primary view of Performance of JP-4 fuel with fluorine-oxygen mixtures in 1000-pound-thrust rocket engines
Nored, Donald L. & Douglass, Howard W.
June 11, 1958
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 Preliminary Analysis of a Nuclear-Powered Supersonic Airplane Using Ramjet Engines
Weber, Richard J. & Connolley, Donald J.
April 11, 1958
Primary view of Free-spinning-tunnel investigation of a 1/28-scale model of the North American FJ-4 airplane: TED No. NACA AD-3112
Healy, Frederick M.
February 11, 1958
Primary view of Investigation of Incipient Spin Characteristics of a 1/35-Scale Model of the Convair F-102A Airplane, Coord. No. AF-AM-79
Healy, Frederick M.
February 11, 1958
Primary view of Performance Evaluation of Reduced-Chord Rotor Blading as Applied to J73 Two-Stage Turbine
Schum, Harold J.
July 11, 1957
Primary view of Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine 1: over-all performance with standard rotor blading at inlet conditions of 35 inches of mercury absolute and 700 degrees R
Berkey, William E.; Rebeske, John J., Jr. & Forrette, Robert E.
July 11, 1957
Primary view of Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine 2: over-all performance at inlet conditions of 35 inches of mercury absolute and 700 degrees R
Schum, Harold J.; Rebeske, John J., Jr. & Forrette, Robert E.
July 11, 1957
Primary view of Performance Evaluation of Reduced-Chord Rotor Blading as Applied to J73 Two-Stage Turbine 6: Stage Performance With Standard Rotor Blading at Inlet Conditions of 35 Inches of Mercury Absolute and 700 Degrees R
Davison, Elmer H. & Schum, Harold J.
July 11, 1957
Primary view of Design and Investigation of a Transonic Axial-Flow Compressor Rotor With an Inlet Hub-Tip Radius Ratio of Essentially Zero
Westphal, Willard R. & Maynard, John W., Jr.
March 11, 1957
Primary view of Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39
Matranga, Gene J. & Peele, James R.
March 11, 1957
Primary view of The influence of imperfect radar space stabilization on the final attack phase of an automatic interceptor system
Triplett, William C.; McLean, John D. & White, John S.
March 11, 1957
Primary view of Preliminary investigation of the combustion of a 50 percent pentaborane - 50 percent JP-4 fuel blend in a turbojet combustor at simulated altitude conditions
Branstetter, J. Robert; Kaufman, Warner B. & Gibbs, James B.
March 11, 1957
Primary view of Aerodynamic heating of a wing as determined from a free-flight rocket-model test to Mach number 3.64
Swanson, Andrew G. & Rumsey, Charles B.
September 11, 1956
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