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Refinado por: data de publicação: Antes de1960 remover tipo de recurso: Reports remover
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11
Subject Headings for Index of NACA Publications
Subject Headings for Index of NACA Publications
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Subject Headings for Index of NACA Publications

Legacy CDMS 1949

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12
Subject Headings for Index of NACA Publications
Subject Headings for Index of NACA Publications
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Subject Headings for Index of NACA Publications

Legacy CDMS 1947

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13
AN EXPLORATORY STUDY OF THE FRENCH CABINETS OF THE FIRST LEGISLATURE OF THE FOURTH REPUBLIC-RESEARCH IN COHESIVE AND DISRUPTIVE TENDENCIES IN COALITION-TYPE GROUPS
AN EXPLORATORY STUDY OF THE FRENCH CABINETS OF THE FIRST LEGISLATURE OF THE FOURTH REPUBLIC-RESEARCH IN COHESIVE AND DISRUPTIVE TENDENCIES IN COALITION-TYPE GROUPS
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AN EXPLORATORY STUDY OF THE FRENCH CABINETS OF THE FIRST LEGISLATURE OF THE FOURTH REPUBLIC-RESEARCH IN COHESIVE AND DISRUPTIVE TENDENCIES IN COALITION-TYPE GROUPS

HOLT, ROBERT

1953

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14
Meddelelser fra Det Norske Myrselskap 1907
Meddelelser fra Det Norske Myrselskap 1907
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Meddelelser fra Det Norske Myrselskap 1907

Thaulow, J. G.

Det Norske Myrselskap 1907

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15
APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 3 TO 4 UTILIZING A DELTA-WING INTERCEPTOR AIRPLANE
APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 3 TO 4 UTILIZING A DELTA-WING INTERCEPTOR AIRPLANE
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APPROACH AND LANDING INVESTIGATION AT LIFT-DRAG RATIOS OF 3 TO 4 UTILIZING A DELTA-WING INTERCEPTOR AIRPLANE

Matranga, G. J. ; Menard, J. A.

Legacy CDMS 1959

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16
Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86
Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86
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Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86

Fetterman, D. E., Jr

Legacy CDMS 1959

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17
WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01
WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01
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WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01

Smith, F. M.

Legacy CDMS 1959

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18
Aerodynamic Characteristics of the X-15/B-52 Combination
Aerodynamic Characteristics of the X-15/B-52 Combination
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Aerodynamic Characteristics of the X-15/B-52 Combination

Alford, W. J., Jr ; Taylor, R. T.

Legacy CDMS 1959

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19
FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL
FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL
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FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL

Andrews, W. H. ; Rediess, H. A.

Legacy CDMS 1959

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20
STATIC STABILITY AND CONTROL OF HYPERSONIC GLIDERS
STATIC STABILITY AND CONTROL OF HYPERSONIC GLIDERS
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STATIC STABILITY AND CONTROL OF HYPERSONIC GLIDERS

Rainey, R. W.

Legacy CDMS 1958

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