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Tests on Built-Up Airplane Struts Having Initial Tension in Outside Fibers

Schwamb, T A / Smith, C S | NTRS | 1923

Point drag and total drag of navy struts no. 1 modified

Zahm, A F / Smith, R H / Hill, G C | NTRS | 1923

Application of electric propulsion to double-ended ferry-boats

Kennedy, A. / Smith, Frank V. | IEEE | 1925

Application of electric propulsion to double-ended ferry boats

Kennedy, Jr., A. / Smith, F.V. | Engineering Index Backfile | 1925

Air Forces, Moments and Damping on Model of Fleet Airship Shenandoah

Zahm, A F / Smith, R H / Louden, F A | NTRS | 1926

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

The Chemical Action of Oils on Single Crystals of Metals

Gwathmey, A T / Leidheiser, H / Smith, G P | NTRS | 1945

Nuclear-Powered Flight. Chapter 1: Introduction and Summary

A. E. Ruark / A. C. Beer / E. A. Bonney et al. | NTIS | 1947

Stress distribution in a beam of orthotropic material subjected to a concentrated load

Smith, C B / Voss, A W | NTRS | 1948

Flight tests of apparatus for varying dihedral effect in flight

Kauffman, W.M. / Smith, A. / Liddell, Jr., C.J. et al. | Engineering Index Backfile | 1948

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10 6 to 11.0 x 10 6

Schaefer, Raymond F. / Smith, Hamilton A. | TIBKAT | 1949

Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

Schaefer, Raymond F / Smith, Hamilton A | NTRS | 1949

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10 6 to 9.0 x 10 6

Loftin, Laurence K. / Smith, Hamilton A. | TIBKAT | 1949

Two-dimensional Aerodynamic Characteristics of 34 Miscellaneous Airfoil Sections

Loftin, Laurence K , Jr / Smith, Hamilton A | NTRS | 1949

Aerodynamic Characteristics of 15 NACA Airfoil Sections at Seven Reynolds Numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

Loftin, Laurence K , Jr / Smith, Hamilton A | NTRS | 1949

Aerodynamic characteristics at Reynolds numbers of 3.0 x 10 6 and 6.0 x 10 6 of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

Smith, Hamilton A. / Schaefer, Raymond F. | TIBKAT | 1950

Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of Three Airfoil Sections Formed by Cutting off Various Amounts from the Rear Portion of the NACA 0012 Airfoil Section

Smith, Hamilton A / Schaefer, Raymond F | NTRS | 1950

Apparatus for varying effective dihedral in flight with application to study of tolerable dihedral on conventional fighter airplane

Kauffman, W.M. / Liddell, Jr., C.J. / Smith, A. et al. | Engineering Index Backfile | 1950

Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in an Unaccelerated Stall and in Pull-ups at Mach Numbers of 0.74, 0.75, 0.94, and 0.97

Smith, Lawrence A | NTRS | 1951

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40

Smith, Norman F / Kainer, Julian H / Webster, Robert A | NTRS | 1951

Thermal Shock Resistance and High-temperature Strength of a Molybdenum Disilicide - Aluminum Oxide Ceramic

Maxwell, W A / Smith, R W | NTRS | 1953

An exploratory investigation of some midcourse guidance systems for the return from the moon

Smith, G. A. | NTRS | 1960

Experimental and theoretical study of a rectangular wing in a vortical wake at low speed

Smith, Willard G. / Lazzeroni, Frank A. | TIBKAT | 1960

SURVEYS OF THE DISTANT GEOMAGNETIC FIELD- PIONEER I AND EXPLORER VI

Sems, A. R. / Smith, E. J. / Sonnett, C. P. | NTRS | 1960

A flight evaluation of an airborne physiological instrumentation system, including preliminary results under conditions of varying accelerations

Smedal, Harald A. / Holden, George R. / Smith, Joseph R. | TIBKAT | 1960

BLUE CLEARING DURING THE 1960-61 MARS APPARITION

Smith, B. A. | NTRS | 1961

The Recovery of Flight Test Payloads

A. M. Smith / R. F. Peck | NTIS | 1961

STUDY OF SELF-EVALUATING STATE VECTOR CONTROL WITH APPLICATIONS TO FLEXIBLE LIQUID-FUELED AERIAL AND SPACE VEHICLES.

Harvey, C. A. / Lee, E. B. / Lovingood, J. A. et al. | NTRS | 1961

THE APPLICATION OF DYNAMIC PROGRAMMING TO OPTIMIZING THE ORBITAL CONTROL PROCESS OF A 24-HOUR COMMUNICATION SATELLITE

Burkhardt, J. A. / Smith, F. T. | NTRS | 1962

THE APPLICATION OF DYNAMIC PROGRAMMING TO OPTIMIZING THE ORBITAL CONTROL PROCESS OF A 24-HOUR COMMUNICATION SATELLITE

Burkhart, J. A. / Smith, F. T. | NTRS | 1962

AN APPLICATION OF TIME OPTIMAL CONTROL TO A FLEXIBLE LAUNCH VEHICLE

Lovingood, J. A. / Smith, F. B., Jr. | NTRS | 1962

PHYSIOLOGICAL INSTRUMENTATION SYSTEMS FOR MONITORING PILOT RESPONSE TO STRESS AT ZERO AND HIGH G

Holden, G. R. / Smedal, H. A. / Smith, J. R., Jr. | NTRS | 1962

Lunar and Planetary Sciences in Space Exploration

Anderson, H. R. / Conel, J. E. / Eimer, M. et al. | NTRS | 1962

The Saturn Program

Von Braun, Wernher / Gilruth, Robert R. / Canright, Richard B. et al. | NTRS | 1962

SPACE ELECTRIC POWER SYSTEMS STUDY FIRST QUARTELY

Bucci, N. W., Jr. / Dobler, F. X. / Doughman, C. L. et al. | NTRS | 1962

The manned lunar base

Smith, G. A. | NTRS | 1963

APPLICATION OF DYNAMIC PROGRAMMING TO OPTIMIZING THE ORBITAL CONTROL PROCESS OF A 24-HOUR COMMUNICATION SATELLITE

Burkhart, J. A. / Smith, F. J. | NTRS | 1963

An application of time-optimal control theory to launch vehicle regulation

Smith, F. B. / Lovingood, J. A. | TIBKAT | 1963

MARTIAN ENTRY CAPSULE- DESIGN CONSIDERATIONS FOR TERMINAL DECELERATION

Mc Mullen, J. C. / Smith, A. M. | NTRS | 1963

Solution of Prandtl's boundary-layer equations

Smith, A. M. O. / Clutter, Darwin W. | TIBKAT | 1963

THE PHYSIOLOGICAL LIMITATIONS OF PERFORMANCE DURING ACCELERATION

Duane, T. D. / Holden, G. R. / Rogers, T. A. et al. | NTRS | 1963

THE MISSION OF MARINER II- PRELIMINARY OBSERVATIONS

Alexander, W. M. / Anderson, H. R. / Coleman, P. J., Jr. et al. | NTRS | 1963

Application of dynamic programming to optimizing the orbital control process of a 24 hour communication satellite

Burkhart, J. A. / Smith, F. T. | NTRS | 1964

A high accuracy instrumentation system with on- line data processing for static rocket test firing.

Choate, E. S. / Sherman, A. / Smith, W. V. | NTRS | 1964

APOLLO Spacecraft Gaseous Nitrogen Deluge System

T. A. Lallas / D. T. Norton / D. C. Smith | NTIS | 1964

Apollo Spacecraft Gaseous Nitrogen Deluge System

Lallas, T. A. / Norton, D. T. / Smith, D. C. | NTRS | 1964

Aerospace vehicle actuation systems studies

Lukase, T. A. / Schissell, G. Z. / Smith, R. M. | NTRS | 1964

Preliminary test results on a compressed multilayer insulation system for a liquid- hydrogen-fueled rocket.

Colaluca, M. A. / Perkins, P. J. / Smith, L. S. | NTRS | 1964

Utilization of acceptance data in a descriptive model for determining manś role in a system

Price, Harold E. / Smith, Edwart E. / Behan, Richard A. | TIBKAT | 1964

Protein, energy, and water requirements of man under simulated space stresses

Homer, G. / Kitzes, G. / Prince, A. E. et al. | NTRS | 1964

Dynamic simulators for test of space vehicle attitude control systems.

Smith, G. A. | NTRS | 1965