|
|
|
|
|
|
Selected Navigations:
Item/Media Type >
[x]
|
Sort results by:
|
|
|
There are a total of 16635 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
|
Calculated performance of a direct-air nuclear turbojet-powered airplane using a split-flow reactor and a separated-type shield
Author(s): Doyle, R. B.
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1951
Added to NTRS: 2008-07-24
Accession Number: 71N70548; Document ID: 19710065235; Report Number: NACA-RM-E50K06
Free flight investigation at transonic speeds of the power-on characteristics including some effects of sonic propulsive jets of a four engine delta wing configuration
Author(s): Falanga, R. A.; Judd, J. H.
Abstract: No Abstract Available
NASA Center: Langley Research Center Publication Year: 1957
Added to NTRS: 2008-07-24
Accession Number: 71N73439; Document ID: 19710068125; Report Number: NACA-RM-L57E31
Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane
Author(s): Koven, William
Abstract: No Abstract Available
NASA Center: Langley Research Center Publication Year: 1946
Added to NTRS: 2008-07-24
Accession Number: 93R21880; Document ID: 19930092590; Report Number: NACA-ARR-L5H11a, NACA-WR-L-99
Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution
Author(s): Seiff, Alvin; Sommer, Simon C; Canning, Thomas N
Abstract: No Abstract Available
NASA Center: Ames Research Center Publication Year: 1957
Added to NTRS: 2008-07-24
Accession Number: 93R19613; Document ID: 19930090323; Report Number: NACA-RM-A56I05
Drag Measurements on Equivalent Bodies of Revolution of Six Configurations of the Convair MX-1964 (Originally MX-1626) Proposed Supersonic Bomber
Author(s): Hall, James Rudyard
Abstract: Tests on equivalent bodies of revolution of six configurations of the Consolidated Vultee Aircraft Corporation proposed supersonic bomber (Convair MX-1964) have indicated that it is possible to reduce the drag of the ...
NASA Center: Langley Research Center Publication Year: 1953
Added to NTRS: 2008-07-24
Document ID: 19990014470; Report Number: L-82024, NACA-RM-SL53K04
Analysis of low-temperature nuclear-powered ramjet missile for high altitudes
Author(s): Rom, F. E.; Sams, E. W.
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1955
Added to NTRS: 2008-07-24
Accession Number: 71N72108; Document ID: 19710066794; Report Number: NACA-RM-E55G21
An investigation of ejection releases of submerged and semisubmerged dynamically scaled stores from a simulated bomb bay of a fighter- bomber airplane at supersonic speeds
Author(s): Carter, H. S.; Lee, J. B.
Abstract: No Abstract Available
NASA Center: Langley Research Center Publication Year: 1956
Added to NTRS: 2008-07-24
Accession Number: 70N72633; Document ID: 19700072930; Report Number: NACA-RM-L56I10
Experimental investigation of laminar-boundary-layer control on an airfoil section equipped with suction slots located at discontinuities in the surface pressure distribution
Author(s): Horton, E. A.; Loftin, L. K., Jr.
Abstract: No Abstract Available
NASA Center: Langley Research Center Publication Year: 1953
Added to NTRS: 2008-07-24
Accession Number: 71N70621; Document ID: 19710065308; Report Number: NACA-RM-L53J14
Measurement of static forces on internally carried bombs of three fineness ratios in flow field of a swept-wing fighter-bomber configuration at a Mach number of 1.61 with illustrative drop path calculations
Author(s): Carlson, H. W.; Smith, N. F.
Abstract: No Abstract Available
NASA Center: Langley Research Center Publication Year: 1957
Added to NTRS: 2008-07-24
Accession Number: 70N72461; Document ID: 19700072759; Report Number: NACA-RM-L56118
Heat exchanger core weights for use with hydrogen expansion turbine
Author(s): Reynolds, T. W.
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1957
Added to NTRS: 2008-07-24
Accession Number: 71N75112; Document ID: 19710069798; Report Number: NACA-RM-E57H09
|
|
|
|
|