|
|
1.
|
HEAT-TRANSFER TESTS OF 20-MILLIMETER PROJECTILES AT A MACH NUMBER OF 5 WITH AN ANALYSIS BY UNSTEADY SCALING LAWS TO PREDICT COMPONENT TEMPERATURE RISES AFTER FIRING FOR VARIOUS FREE -FLIGHT CONDITIONS
by Trimpi,Robert L, Gallagher,James G | Jones,Robert A. Material type:  Book Description: 30.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-758 -] (1).
|
|
|
2.
|
A PERFECT-GAS ANALYSIS OF THE EXPANSION TUNNEL, A MODIFICATION TO THE EXPANSION TUBE
by Trimpi,Robert L | Callis,Linwood B. Material type: Book Description: 101.Publisher: Nasa, Washington, D.C. 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TR R-223] (1).
|
|
|
3.
|
A NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON
by Trimpi,Robert L | Cohen,Nathaniel B. Material type: Book Description: 55.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TR R-85] (1).
|
|
|
4.
|
A THEORETICAL INVESTIGATION OF SIMULATION IN EXPANSION TUBES AND TUNNELS
by Trimpi,Robert L. Material type: Book Description: 59.Publisher: Nasa, Washington, D.C. 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TR R-243] (1).
|
|
|
5.
|
Heat transfer tests of 20 millimeter projectiles at a mach number of 5 with an analysis by unsteady scaling laws to predict component temperature rises after firing for various free flight conditions [NASA TN D751-TN D760]
by Trimpi, Robert L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 30p.Publisher: Washington National Aeronautics and Space Administration [NASA] 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
6.
|
A method of solution with tabulated results for the attached oblique shock wave system for surfaces at various angles of attack, sweep, and dihedral in an equilibrium real gas including the atmosphere [ NASA TR R-63]
by Trimpi, Robert L | Jones, Robert A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 141p.Publisher: Washington, D.C.. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
|
|
7.
|
Transient temperature distribution in two component semi infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat transfer coefficient [Technical Note 4308]
by Trimpi, Robert L | Jones, Robert A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 83p.Publisher: Washington National Advisory Committee for Aeronautics 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
