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Peter F. Intrieri
Observed names:
Intrieri, Peter F.,
P. F. Intrieri,
P. INTRIERI,
PETER F. INTRIERI,
Pete Intrieri
Institution:
Ames Research Center
Observed institutions:
Ames Research Center,
Eloret (United States)
OpenAlex ID:
A5083820161
High-speed aerodynamics of several blunt-cone configurations
1987
·
Peter F. Intrieri
, Donn B. Kirk
·
Journal of Spacecraft and Rockets
·
36
Structure of the Atmosphere of Venus up to 110 Kilometers: Preliminary Results from the Four Pioneer Venus Entry Probes
1979
·
Alvin Seiff
, Donn B. Kirk
, et al.
·
Science
·
31
Flight characteristics of probes in the atmospheres of Mars, Venus and the outer planets
1977
·
Peter F. Intrieri
, Charles E. De Rose
, et al.
·
Acta Astronautica
·
28
Aerodynamic Behavior of the Viking Entry Vehicle: Ground Test and Flight Results
1978
·
Donn B. Kirk
, Peter F. Intrieri
, et al.
·
Journal of Spacecraft and Rockets
·
26
Ballistic Range Investigation of Sonic-Boom Overpressures in Water
1973
·
PETER F. INTRIERI
, GERALD N. MALCOLM
·
AIAA Journal
·
24
Ballistic range tests of ablating and nonablating slender cones
1970
·
PETER F. INTRIERI
, DONN B. KIRK
, et al.
·
AIAA Journal
·
14
Galileo probe aerodynamics
1996
·
Alvin Seiff
, Ethiraj Venkatapathy
, et al.
·
AIAA Applied Aerodynamics Conference
·
11
Ballistic range investigation of sonic-boom overpressures in water
1972
·
G. MALCOLM
, P. INTRIERI
·
AIAA Advanced Marine Vehicles Conference
·
7
Aerodynamic behavior of the Viking entry vehicle - Ground test and flight results
1977
·
D. KIRK
, P. INTRIERI
, et al.
·
Guidance and Control Conference
·
3
Flight characteristics of probes in the atmospheres of Mars, Venus, and the outer planets
1976
·
P. F. Intrieri
, C. E. Derose
, et al.
·
NASA Technical Reports Server (NASA)
·
3
Study of the stability and drag at mach numbers from 4.5 to 13.5 of a conical venus- entry body
1965
·
P. F. Intrieri
·
NASA Technical Reports Server (NASA)
·
3
PDF
High-speed aerodynamics of several blunt-cone configurations
1986
·
P. INTRIERI
, D. KIRK
·
24th Aerospace Sciences Meeting
·
2
Ablation testing in ballistic ranges
1968
·
P. INTRIERI
, D. KIRK
·
AIAA Aerodynamic Measurement Technology and Ground Testing Conference
·
2
Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air
1966
·
P. F. Intrieri
·
NASA Technical Reports Server (NASA)
·
1
Experimental investigation of hypersonic aerodynamics
1987
·
P. F. Intrieri
·
NASA Technical Reports Server (NASA)
PDF
Ballisistic range measurements of the drag and static and dynamic stability of a recoverable space shuttle booster vehicle
1972
·
P. F. Intrieri
, Donn B. Kirk
·
NASA STI Repository (National Aeronautics and Space Administration)
Static and dynamic aerodynamics of space shuttle vehicles
1971
·
John A. Axelson
, J. J. Brownson
, et al.
·
NASA Technical Reports Server (NASA)
Effects of transverse center-of-gravity displacement, afterbody geometry, and front-face curvature on the aerodynamic characteristics of Mercury-type models at a Mach number of 5.5
1961
·
P. F. Intrieri
·
NASA Technical Reports Server (NASA)
PDF
Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models
1957
·
P. F. Intrieri
, Willard G Smith
·
NASA Technical Reports Server (NASA)
PDF
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Works count:
20
Citation count:
191
H-index:
7
I10-index:
7
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