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4921.
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ROTATIONAL-TEMPERATURE DETERMINATION IN FLOWING NITROGEN USING AN ELECTRON BEAM.
by Lillicrap,D C | Lee,L P. Material type:  Book Description: 31.Publisher: Nasa, Washington, D.C. 1971Availability: No items available
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4922.
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VOLTAGE-PROGRAMED CONTROL OF TURBOALTERATOR LOAD.
by Young,Richard N | Kelsey,Eugene L. Material type: Book Description: 11.Publisher: Nasa, Washington, D.C. 1971Availability: No items available
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4923.
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THE DESIGN OF SAILPLANES FOR OPTIMUM THERMAL SOARING PERFORMANCE.
by Cone,Clarence D. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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4924.
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WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.
by Henning,Allen B,Lundstrom,Reginald R | Keating,Jean C. Material type: Book Description: 81.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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4925.
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STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.
by Young,John W. Material type: Book Description: 45.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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4926.
|
PHENOMENA OF PNEUMATIC TIRE HYDROPLANNING.
by Horne,Walter B | Dreher,Robert C. Material type: Book Description: 52.Publisher: Nasa, Washington, D.C. 1963Availability: No items available
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4927.
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STATIC LONGITUDINAL CHRACTERISTICS OF THE PROJECT FIRE REENTRY STAGE AFTER REENTRY-PACKAGE SEPRATION AT MACH 28.3 IN HELIUM.
by Snyder,Curtlis D. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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4928.
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APPROXIMATE CALCULATION OF HYPERSONIC CONICAL FLOW PARAMETERS FOR AIR IN THERMODYNAMICS EQUILIBRIUM.
by Newman,Perry A. Material type: Book Description: 15.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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4929.
|
IMPORTANT STRUCTURAL RESEARCH PROBLEMS FOR THE SUPPORT OF FUTURE SPACE MISSIONS.
by Abraham,Lewis H. Material type: Book Description: 16.Publisher: Nasa, Washington, D.C. 1963Availability: No items available
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4930.
|
A PILOTED SIMULATOR STUDY OF THE LOSS OF ALTITUDE BY JET TRANSPORT IN A GO-AROUND FROM AN INSTRUMENT-LANDING APPOACH.
by Mcnei Ll,Walter E. Material type: Book Description: 28.Publisher: Nasa, Washington, D.C. 1963Availability: No items available
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4931.
|
ANALYSIS OF PRESSURIZED AND AXIALLY LOADED ORTHOTROPIC MULTICELL TANKS
by Blum,Robert E. Material type: Book Description: 18.Publisher: Nasa, Washington, D.C. 1965Availability: No items available
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4932.
|
EFFECT OF UNIFORM LONGITUDINAL STRAIN RATE ON WEAK HOMOGENEOUS TURBULENCE IN A COMPRESSIBLE FLOW
by Deissler,Robert G. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1965Availability: No items available
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4933.
|
WAKE MEASUREMENTS BEHIND A WING SECTION OF A FIGHTER AIRPLANES IN FAST DIVES.
by Beeler,De E | Gerard,George. Material type: Book Publisher: Nasa, Washington, D.C. 1947Availability: No items available
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4934.
|
MEASURED AND THEORETICAL FLOW FIELDS BEHIND A RETANGULAR AND A TRIANGULAR WING UP TO HIGH ANGLES OF AATACK AT A MACH NUMBER OF 2.46.
by Centolanzi,Frank J. Material type: Book Description: 76.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4935.
|
APPLICATIOIN TO FLUID DYNAMIC OF THE THEORY OF REVERSIBLE HEAT ADDITION.
by Baldwin,Barrett S. Material type: Book Description: 18.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4936.
|
INVESTIGATION OF HIGH-SPEED IMPACT
: REGIONS OF IMPACT AND IMPACT AT OBLIQUE ANGLES.
by Summers,James L. Material type: Book Description: 18.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4937.
|
THEORETICAL ANALYSIS OF THE CREEP COLLAPSE OF COLUMNS.
by Schlechte,Floyed R. Material type: Book Description: 46.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4938.
|
A METHOD FOR CALCULATING AERODYNAMICS LOADING ON THE WINGS AT A MACH NUMBER OF 1.
by Crigler,John L. Material type: Book Description: 96.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4939.
|
A NOTE ON THE CALCULATION OF HELICOPTER PERFORMANCE AT HIGH TIP-SPEED RATIOS.
by Gessow,Alfred. Material type: Book Description: 13.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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4940.
|
OPTIMUM PROPORTIONS OF TRUSS-CORE AND WEB-CORE SANDWICH PLATES LOADED IN COMPRESSION.
by Anderson,Mevin S. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1959Availability: No items available
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