NAS 1.26:1796
|
Subsonic static characteristics of slender wing configurations using a magnetic suspension and balance system / |
1 |
NAS 1.26:1797
|
Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations / |
1 |
NAS 1.26:1798
|
Techniques for generation of control and guidance signals derived from optical fields : Part II / |
1 |
NAS 1.26:1799
|
High temperature capacitor development / |
1 |
NAS 1.26:1800
|
Imperfection sensitivity of optimum structural designs for a Mars entry capsule / |
1 |
NAS 1.26:1801
|
Computer program for analysis of imperfection sensitivity of ring stiffened shells of revolution / |
1 |
NAS 1.26:1802
|
Composition and concentrative properties of human urine / |
1 |
NAS 1.26:1803
|
Design and experimental results of a highly loaded, low solidity tandem rotor / |
1 |
NAS 1.26:1804
|
Radiation measurements and low frequency and high pressure investigations of induction heated plasma / |
1 |
NAS 1.26:1805
|
Joint determination of orbits of spacecraft and moons of Mars by optical sighting of the moons / |
1 |
NAS 1.26:1806
|
General dynamics of the physical-chemical systems in mammals / |
1 |
NAS 1.26:1807
|
Institutional factors in civil aviation / |
1 |
NAS 1.26:1808/
|
A historical study of the benefits derived from application of technical advances to civil aviation. |
1 |
NAS 1.26:1809/
|
A historical study of the benefits derived from application of technical advances to civil aviation. |
1 |
NAS 1.26:1810
|
Refractory metal valves for 1900 deg F service in alkali metal systems / |
1 |
NAS 1.26:1811
|
Corrosion resistance of tantalum, T 111, and Cb-1Zr to mercury at 1200 F / |
1 |
NAS 1.26:1812
|
Development of a heat-sterilizable 40-Ah sealed silver-zinc cell / |
1 |
NAS 1.26:1813
|
Development and endurance testing of high-temperature ceremic voltage-regulator tubes / |
1 |
NAS 1.26:1814
|
A review of the output performance of six planar thermionic converters with various electrode materials / |
1 |
NAS 1.26:1815
|
Three stage potassium vapor turbine test / |
1 |