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Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Investigation of Wingless Missile Configurations with Folding Controls and Low-Aspect-Ratio Stabilizing Surfaces
Lazzeroni, Frank A.
September 17, 1958
Primary view of Measurements of the Buffeting Loads on the Wing and Horizontal Tail of a 1/4-Scale Model of the X-1E Airplane
Rainey, A. Gerald & Igoe, William B.
September 17, 1958
Primary view of Stability Investigation of a Blunt Cone and a Blunt Cylinder With a Square Base at Mach Numbers From 0.64 to 2.14
Coltrane, Lucille C.
September 17, 1958
Primary view of Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile
Winovich, Warren & Higdon, Nancy S.
July 17, 1958
Primary view of Heat-Transfer Measurements on a Concave Hemispherical Nose Shape With Unsteady-Flow Effects at Mach Numbers of 1.98 and 4.95
Cooper, Morton; Beckwith, Ivan E.; Jones, Jim J. & Gallagher, James J.
July 17, 1958
Primary view of Simulator Investigation of Command Reaction Controls
Holleman, Euclid C. & Stillwell, Wendell H.
July 17, 1958
Primary view of Some Altitude Operational Characteristics of a Prototype Iroquois Turbojet Engine, COORD. NO. AF-P-6
Peters, Daniel J. & McAulay, John E.
June 17, 1958
Primary view of Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities
Schmidt, Harold W.
April 17, 1958
Primary view of Incipient spin characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA AD 3118
Healy, Frederick M.
April 17, 1958
Primary view of An Analog Study of the Influence of Internal Modifications to a Wing Leading Edge on Its Transient Temperature Rise During Highspeed Flight
Neel, Carr B.
March 17, 1958
Primary view of Section Thrust Coefficients for a Full-Scale, Three-Blade, Supersonic-Type Propeller Operating at Low and Negative Blade Angles
Salters, Leland B., Jr. & Lewis, Martha C.
March 17, 1958
Primary view of Two-dimensional cascade investigation at Mach numbers up to 1.0 of NACA 65-series blade sections at conditions typical of compressor tips
Dunavant, James C. & Emery, James C.
March 17, 1958
Primary view of Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: longitudinal characteristics of an unswept wing and canard
Peterson, Victor L. & Boyd, John W.
February 17, 1958
Primary view of Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22longitudinal characteristics of a triangular wing and unswept canard
Peterson, Victor L. & Menees, Gene P.
February 17, 1958
Primary view of Transonic Investigation of an Axial-Flow Compressor Rotor With a Contracted Exit Annulus
Babington, Robert S.
February 17, 1958
Primary view of Aerodynamic Performance of Several Techniques for Spike-Position Control of a Blunt-Lip Nose Inlet Having Internal Contraction; Mach Numbers of 0.63 and 1.5 to 2.0
Anderson, Arthur A. & Weinstein, Maynard I.
September 17, 1957
Primary view of Flight Investigation of Pentaborane Fuel in Rocket Boosted 9.75-Inch-Diameter Ramjet Engine With Convergent-Divergent Exhaust Nozzle
Disher, John H.
September 17, 1957
Primary view of Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 3: experimental performance with two stator configurations designed to eliminate blade wakes and secondary-flow effects and conclusions from entire sta
Rohlik, Harold E.; Wintucky, William T. & Moffitt, Thomas P.
September 17, 1957
Primary view of Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 3 - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-Flow Effects and Conclusions From Entire Stator Investigation
Rohlik, Harold E.; Wintucky, William T. & Moffitt, Thomas P.
September 17, 1957
Primary view of Investigation of Ejection Releases of an MB-1 Rocket From a 0.04956-Scaled Model of the Convair F-106A Airplane at Several Mach Numbers and Simulated Altitudes
Lee, John B. & Basford, Robert C.
September 17, 1957
Primary view of Investigation of Ejection Releases of an MB-1 Rocket From a 0.04956-Scaled Model of the Convair F-106A Airplane at Several Mach Numbers and Simulated Attitudes : Coord. No. AF-AM-57
Lee, John B. & Basford, Robert C.
September 17, 1957
Primary view of A Semiempirical Correlation of Afterburner Combustion Efficiency and Lean-Blowout Fuel-Air-Ratio Data with Several Afterburner-Inlet Variables and Afterburner Lengths
King, Charles R.
September 17, 1957
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